LINUSS2 is a payload in GEO orbit, operated by Lockheed Martin Space Systems (Denver), Astronautics Operations, launched 2022.
Orbital data last updated 3 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | GEO |
| Inclination | 5.4200° |
| Eccentricity | 0.0007570 |
| Period | 1453.7 min |
| Apogee | 36,164 km |
| Perigee | 36,099 km |
| Mean motion | 0.99054468 rev/day |
| RAAN | 64.0464° |
| Arg of perigee | 317.6612° |
| Mean anomaly | 215.9306° |
| B* | 0.0000e+0 |
| Rev at epoch | 1,188 |
1 55247U 22144H 26185.44689860 -.00000268 00000-0 00000-0 0 99902 55247 5.4200 64.0464 0007570 317.6612 215.9306 0.99054468 11884{
"OBJECT_NAME": "LINUSS2",
"OBJECT_ID": "2022-144H",
"EPOCH": "2026-07-04T10:43:32.039+00:00",
"MEAN_MOTION": 0.99054468,
"ECCENTRICITY": 0.000757,
"INCLINATION": 5.42,
"RA_OF_ASC_NODE": 64.0464,
"ARG_OF_PERICENTER": 317.6612,
"MEAN_ANOMALY": 215.9306,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 55247,
"REV_AT_EPOCH": 1188,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000268,
"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 | LINUSS2 |
| Operator | Lockheed Martin Space Systems (Denver), Astronautics OperationsHIGHvia GCAT — Jonathan McDowell's General Catalog |
| 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 |