LEMUR-2-MJR092620 is a payload in SSO orbit, operated by Spire/Glasgow / GHGSat Inc., launched 2023.
| Orbit class | SSO |
| Inclination | 97.3969° |
| Eccentricity | 0.0006071 |
| Period | 93.2 min |
| Apogee | 434 km |
| Perigee | 425 km |
| Mean motion | 15.45636987 rev/day |
| RAAN | 278.1135° |
| Arg of perigee | 58.6351° |
| Mean anomaly | 301.5491° |
| B* | 3.1298e-4 |
| Rev at epoch | 14,866 |
1 58340U 23174CN 26187.71556336 .00015007 00000-0 31298-3 0 99962 58340 97.3969 278.1135 0006071 58.6351 301.5491 15.45636987148666{
"OBJECT_NAME": "LEMUR-2-MJR092620",
"OBJECT_ID": "2023-174CN",
"EPOCH": "2026-07-06T17:10:24.674+00:00",
"MEAN_MOTION": 15.45636987,
"ECCENTRICITY": 0.0006071,
"INCLINATION": 97.3969,
"RA_OF_ASC_NODE": 278.1135,
"ARG_OF_PERICENTER": 58.6351,
"MEAN_ANOMALY": 301.5491,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58340,
"REV_AT_EPOCH": 14866,
"BSTAR": 0.00031298,
"MEAN_MOTION_DOT": 0.00015007,
"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 | LEMUR-2-MJR092620 |
| 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 |