CELESTIS-02 & TAURUS R/B
Launch
Launched on Feb 10, 1998 from Space Launch Complex 576E, United States of America aboard a Minotaur-C 2210.
Taurus 2210 | GFO →Live · TLE epoch 2026-09-08 13:58 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
United States Government
Country
United States
Manufacturer
—
Launched
Feb 10, 1998
Mass
—
Apogee
867 km
Perigee
777 km
Inclination
108.01°
Period
1.69 h
Altitude history
Apogee and perigee for CELESTIS-02 & TAURUS R/B across 14 days of archived orbital elements (15 element sets, one per day).
Trend
Stable
Change
-0.0 km
Rate
-0.00 km/day
Now
777 × 867 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
Launched with
One other catalogued object still in orbit from launch 1998-007 (Taurus 2210 | GFO).
- ORBCOMM FM04 · 25159
Sources & further reading
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