LEMUR-2-JK0903EM1407 is a payload in SSO orbit, operated by Spire/Glasgow / GHGSat Inc., launched 2023.
| Orbit class | SSO |
| Inclination | 97.3914° |
| Eccentricity | 0.0004296 |
| Period | 92.7 min |
| Apogee | 412 km |
| Perigee | 406 km |
| Mean motion | 15.52763120 rev/day |
| RAAN | 279.2419° |
| Arg of perigee | 58.9562° |
| Mean anomaly | 301.2112° |
| B* | 3.3311e-4 |
| Rev at epoch | 14,883 |
1 58336U 23174CJ 26188.19316044 .00020526 00000-0 33311-3 0 99942 58336 97.3914 279.2419 0004296 58.9562 301.2112 15.52763120148836{
"OBJECT_NAME": "LEMUR-2-JK0903EM1407",
"OBJECT_ID": "2023-174CJ",
"EPOCH": "2026-07-07T04:38:09.062+00:00",
"MEAN_MOTION": 15.5276312,
"ECCENTRICITY": 0.0004296,
"INCLINATION": 97.3914,
"RA_OF_ASC_NODE": 279.2419,
"ARG_OF_PERICENTER": 58.9562,
"MEAN_ANOMALY": 301.2112,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58336,
"REV_AT_EPOCH": 14883,
"BSTAR": 0.00033311,
"MEAN_MOTION_DOT": 0.00020526,
"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-JK0903EM1407 |
| Operator | |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |