LEMUR-2-TOMATOKECHUP is a payload in SSO orbit, operated by Spire/Glasgow / Hubble Network Inc., launched 2024.
| Orbit class | SSO |
| Inclination | 97.3789° |
| Eccentricity | 0.0002908 |
| Period | 93.7 min |
| Apogee | 459 km |
| Perigee | 455 km |
| Mean motion | 15.36460405 rev/day |
| RAAN | 269.8148° |
| Arg of perigee | 137.9028° |
| Mean anomaly | 222.2440° |
| B* | 2.5500e-4 |
| Rev at epoch | 10,516 |
1 60471U 24149D 26187.71347409 .00008991 00000-0 25500-3 0 99992 60471 97.3789 269.8148 0002908 137.9028 222.2440 15.36460405105163{
"OBJECT_NAME": "LEMUR-2-TOMATOKECHUP",
"OBJECT_ID": "2024-149D",
"EPOCH": "2026-07-06T17:07:24.161+00:00",
"MEAN_MOTION": 15.36460405,
"ECCENTRICITY": 0.0002908,
"INCLINATION": 97.3789,
"RA_OF_ASC_NODE": 269.8148,
"ARG_OF_PERICENTER": 137.9028,
"MEAN_ANOMALY": 222.244,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 60471,
"REV_AT_EPOCH": 10516,
"BSTAR": 0.000255,
"MEAN_MOTION_DOT": 0.00008991,
"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-TOMATOKECHUP |
| 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 |