ANSER FOLLOWER 2 is a payload in SSO orbit, operated by National Institute of Aerospace Technology, launched 2023.
| Orbit class | SSO |
| Inclination | 97.5509° |
| Eccentricity | 0.0001392 |
| Period | 92.9 min |
| Apogee | 418 km |
| Perigee | 417 km |
| Mean motion | 15.49735484 rev/day |
| RAAN | 277.1435° |
| Arg of perigee | 219.3282° |
| Mean anomaly | 140.7868° |
| B* | 4.1464e-4 |
| Rev at epoch | 15,189 |
1 58018U 23155C 26187.18429226 .00022959 00000-0 41464-3 0 99952 58018 97.5509 277.1435 0001392 219.3282 140.7868 15.49735484151898{
"OBJECT_NAME": "ANSER FOLLOWER 2",
"OBJECT_ID": "2023-155C",
"EPOCH": "2026-07-06T04:25:22.851+00:00",
"MEAN_MOTION": 15.49735484,
"ECCENTRICITY": 0.0001392,
"INCLINATION": 97.5509,
"RA_OF_ASC_NODE": 277.1435,
"ARG_OF_PERICENTER": 219.3282,
"MEAN_ANOMALY": 140.7868,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58018,
"REV_AT_EPOCH": 15189,
"BSTAR": 0.00041464,
"MEAN_MOTION_DOT": 0.00022959,
"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 | ANSER FOLLOWER 2 |
| Operator | |
| Country | Spain |
| 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 |