▸Orbital parameters

Orbit class	LEO
Inclination	52.9788°
Eccentricity	0.0009297
Period	94.7 min
Apogee	510 km
Perigee	497 km
Mean motion	15.20800178 rev/day
RAAN	221.3760°
Arg of perigee	169.9979°
Mean anomaly	190.1202°
B*	-1.7865e-4
Rev at epoch	10,067

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 61046U 24163B 26187.32459635 -.00004321 00000-0 -17865-3 0 9996

2 61046 52.9788 221.3760 0009297 169.9979 190.1202 15.20800178100677

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPACEMOBILE-005",
  "OBJECT_ID": "2024-163B",
  "EPOCH": "2026-07-06T07:47:25.125+00:00",
  "MEAN_MOTION": 15.20800178,
  "ECCENTRICITY": 0.00092973,
  "INCLINATION": 52.9788,
  "RA_OF_ASC_NODE": 221.376,
  "ARG_OF_PERICENTER": 169.9979,
  "MEAN_ANOMALY": 190.1202,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61046,
  "REV_AT_EPOCH": 10067,
  "BSTAR": -0.00017864937,
  "MEAN_MOTION_DOT": -0.00004321,
  "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-005
Operator	Avellan Space Technology and ScienceHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AST SpaceMobileMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Sep 12, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1500HIGH

▸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/61046

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