LEMUR-2-JOHNNYTRUONG is a payload in SSO orbit, operated by Spire/Glasgow / Hubble Network Inc., launched 2024.
| Orbit class | SSO |
| Inclination | 97.5392° |
| Eccentricity | 0.0004383 |
| Period | 92.2 min |
| Apogee | 385 km |
| Perigee | 379 km |
| Mean motion | 15.62060405 rev/day |
| RAAN | 340.9066° |
| Arg of perigee | 117.4425° |
| Mean anomaly | 242.7278° |
| B* | 3.8537e-4 |
| Rev at epoch | 13,112 |
1 59146U 24043BA 26187.95549127 .00033663 00000-0 38537-3 0 99942 59146 97.5392 340.9066 0004383 117.4425 242.7278 15.62060405131121{
"OBJECT_NAME": "LEMUR-2-JOHNNYTRUONG",
"OBJECT_ID": "2024-043BA",
"EPOCH": "2026-07-06T22:55:54.446+00:00",
"MEAN_MOTION": 15.62060405,
"ECCENTRICITY": 0.0004383,
"INCLINATION": 97.5392,
"RA_OF_ASC_NODE": 340.9066,
"ARG_OF_PERICENTER": 117.4425,
"MEAN_ANOMALY": 242.7278,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 59146,
"REV_AT_EPOCH": 13112,
"BSTAR": 0.00038537,
"MEAN_MOTION_DOT": 0.00033663,
"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-JOHNNYTRUONG |
| 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 |