LEMUR-2-DEVERILL-M-T is a payload in SSO orbit, operated by Spire, launched 2023.
| Orbit class | SSO |
| Inclination | 99.4457° |
| Eccentricity | 0.0004826 |
| Period | 93.5 min |
| Apogee | 447 km |
| Perigee | 441 km |
| Mean motion | 15.40798333 rev/day |
| RAAN | 232.5577° |
| Arg of perigee | 332.4144° |
| Mean anomaly | 27.6839° |
| B* | 5.1594e-4 |
| Rev at epoch | 16,430 |
1 57391U 23100F 26188.04906124 .00021057 00000-0 51594-3 0 99942 57391 99.4457 232.5577 0004826 332.4144 27.6839 15.40798333164309{
"OBJECT_NAME": "LEMUR-2-DEVERILL-M-T",
"OBJECT_ID": "2023-100F",
"EPOCH": "2026-07-07T01:10:38.891+00:00",
"MEAN_MOTION": 15.40798333,
"ECCENTRICITY": 0.0004826,
"INCLINATION": 99.4457,
"RA_OF_ASC_NODE": 232.5577,
"ARG_OF_PERICENTER": 332.4144,
"MEAN_ANOMALY": 27.6839,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 57391,
"REV_AT_EPOCH": 16430,
"BSTAR": 0.00051594,
"MEAN_MOTION_DOT": 0.00021057,
"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-DEVERILL-M-T |
| 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 |