CELESTIS-02 & TAURUS R/B is a rocket body in LEO orbit, operated by Orbital Sciences Corp./Chandler, launched 1998.
| Orbit class | LEO |
| Inclination | 108.0159° |
| Eccentricity | 0.0060180 |
| Period | 101.2 min |
| Apogee | 860 km |
| Perigee | 774 km |
| Mean motion | 14.22492129 rev/day |
| RAAN | 11.2225° |
| Arg of perigee | 100.5004° |
| Mean anomaly | 316.5994° |
| B* | 6.5308e-5 |
| Rev at epoch | 47,325 |
1 25160U 98007D 26187.44773065 .00000019 00000-0 65308-4 0 99942 25160 108.0159 11.2225 0060180 100.5004 316.5994 14.22492129473252{
"OBJECT_NAME": "CELESTIS-02 & TAURUS R/B",
"OBJECT_ID": "1998-007D",
"EPOCH": "2026-07-06T10:44:43.928+00:00",
"MEAN_MOTION": 14.22492129,
"ECCENTRICITY": 0.006018,
"INCLINATION": 108.0159,
"RA_OF_ASC_NODE": 11.2225,
"ARG_OF_PERICENTER": 100.5004,
"MEAN_ANOMALY": 316.5994,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 25160,
"REV_AT_EPOCH": 47325,
"BSTAR": 0.000065308,
"MEAN_MOTION_DOT": 1.9e-7,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | CELESTIS-02 & TAURUS R/B |
| Operator | |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | ROCKET_BODYHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |