ASBM-2 is a payload in HEO orbit, operated by Space Norway AS / US Space Force Space Systems Command, launched 2024.
Orbital data last updated 5 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | HEO |
| Inclination | 62.8582° |
| Eccentricity | 0.5617301 |
| Period | 957.3 min |
| Apogee | 43,871 km |
| Perigee | 7,723 km |
| Mean motion | 1.50423767 rev/day |
| RAAN | 44.9742° |
| Arg of perigee | 269.5081° |
| Mean anomaly | 29.4266° |
| B* | 0.0000e+0 |
| Rev at epoch | 1,182 |
1 60423U 24143B 26182.78939448 -.00000098 00000-0 00000-0 0 99982 60423 62.8582 44.9742 5617301 269.5081 29.4266 1.50423767 11828{
"OBJECT_NAME": "ASBM-2",
"OBJECT_ID": "2024-143B",
"EPOCH": "2026-07-01T18:56:43.683+00:00",
"MEAN_MOTION": 1.50423767,
"ECCENTRICITY": 0.5617301,
"INCLINATION": 62.8582,
"RA_OF_ASC_NODE": 44.9742,
"ARG_OF_PERICENTER": 269.5081,
"MEAN_ANOMALY": 29.4266,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 60423,
"REV_AT_EPOCH": 1182,
"BSTAR": 0,
"MEAN_MOTION_DOT": -9.8e-7,
"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 | ASBM-2 |
| Operator | Space Norway AS / US Space Force Space Systems CommandHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 3505HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |