LEMUR-2-HUBBLE-5 is a payload in SSO orbit, operated by Hubble Network Inc. / Spire/Glasgow, launched 2025.
| Orbit class | SSO |
| Inclination | 97.7734° |
| Eccentricity | 0.0004094 |
| Period | 96.4 min |
| Apogee | 588 km |
| Perigee | 582 km |
| Mean motion | 14.94194144 rev/day |
| RAAN | 301.6518° |
| Arg of perigee | 274.4902° |
| Mean anomaly | 85.5850° |
| B* | 1.4618e-4 |
| Rev at epoch | 5,676 |
1 64840U 25135BT 26187.31043794 .00001509 00000-0 14618-3 0 99912 64840 97.7734 301.6518 0004094 274.4902 85.5850 14.94194144 56766{
"OBJECT_NAME": "LEMUR-2-HUBBLE-5",
"OBJECT_ID": "2025-135BT",
"EPOCH": "2026-07-06T07:27:01.838+00:00",
"MEAN_MOTION": 14.94194144,
"ECCENTRICITY": 0.00040937,
"INCLINATION": 97.7734,
"RA_OF_ASC_NODE": 301.6518,
"ARG_OF_PERICENTER": 274.4902,
"MEAN_ANOMALY": 85.585,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 64840,
"REV_AT_EPOCH": 5676,
"BSTAR": 0.00014617556,
"MEAN_MOTION_DOT": 0.00001509,
"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-HUBBLE-5 |
| 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 |