▸Orbital parameters

Orbit class	LEO
Inclination	52.9952°
Eccentricity	0.0010676
Period	94.8 min
Apogee	517 km
Perigee	503 km
Mean motion	15.18643108 rev/day
RAAN	240.0450°
Arg of perigee	189.1004°
Mean anomaly	170.9798°
B*	4.7122e-5
Rev at epoch	2,963

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 67232U 25309A 26188.18193632 .00000667 00000-0 47122-4 0 9996

2 67232 52.9952 240.0450 0010676 189.1004 170.9798 15.18643108 29630

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPACEMOBILE-006",
  "OBJECT_ID": "2025-309A",
  "EPOCH": "2026-07-07T04:21:59.298+00:00",
  "MEAN_MOTION": 15.18643108,
  "ECCENTRICITY": 0.0010676,
  "INCLINATION": 52.9952,
  "RA_OF_ASC_NODE": 240.045,
  "ARG_OF_PERICENTER": 189.1004,
  "MEAN_ANOMALY": 170.9798,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67232,
  "REV_AT_EPOCH": 2963,
  "BSTAR": 0.000047122,
  "MEAN_MOTION_DOT": 0.00000667,
  "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.

▸Satellite metadata

Name	SPACEMOBILE-006
Operator	Avellan Space Technology and ScienceHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AST SpaceMobileMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Dec 24, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5850HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/67232

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.