LEO EXPRESS 2 is a payload in SSO orbit, operated by Impulse Space Propulsion, launched 2025.
| Orbit class | SSO |
| Inclination | 97.3470° |
| Eccentricity | 0.0004131 |
| Period | 94.4 min |
| Apogee | 493 km |
| Perigee | 488 km |
| Mean motion | 15.25165648 rev/day |
| RAAN | 261.8193° |
| Arg of perigee | 115.3088° |
| Mean anomaly | 244.8578° |
| B* | 1.9700e-4 |
| Rev at epoch | 13,963 |
1 62673U 25009BS 26188.14407874 .00004870 00000-0 19700-3 0 99992 62673 97.3470 261.8193 0004131 115.3088 244.8578 15.25165648139634{
"OBJECT_NAME": "LEO EXPRESS 2",
"OBJECT_ID": "2025-009BS",
"EPOCH": "2026-07-07T03:27:28.403+00:00",
"MEAN_MOTION": 15.25165648,
"ECCENTRICITY": 0.0004131,
"INCLINATION": 97.347,
"RA_OF_ASC_NODE": 261.8193,
"ARG_OF_PERICENTER": 115.3088,
"MEAN_ANOMALY": 244.8578,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62673,
"REV_AT_EPOCH": 13963,
"BSTAR": 0.000197,
"MEAN_MOTION_DOT": 0.0000487,
"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 | LEO EXPRESS 2 |
| Operator | |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |