▸Orbital parameters

Orbit class	LEO
Inclination	52.9741°
Eccentricity	0.0007438
Period	94.7 min
Apogee	509 km
Perigee	498 km
Mean motion	15.20820517 rev/day
RAAN	219.8899°
Arg of perigee	169.1843°
Mean anomaly	190.9313°
B*	9.9523e-5
Rev at epoch	10,071

▸Two-line element set (TLE)

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

1 61047U 24163C 26187.58603882 .00001897 00000-0 99523-4 0 9995

2 61047 52.9741 219.8899 0007438 169.1843 190.9313 15.20820517100714

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPACEMOBILE-001",
  "OBJECT_ID": "2024-163C",
  "EPOCH": "2026-07-06T14:03:53.754+00:00",
  "MEAN_MOTION": 15.20820517,
  "ECCENTRICITY": 0.0007438,
  "INCLINATION": 52.9741,
  "RA_OF_ASC_NODE": 219.8899,
  "ARG_OF_PERICENTER": 169.1843,
  "MEAN_ANOMALY": 190.9313,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61047,
  "REV_AT_EPOCH": 10071,
  "BSTAR": 0.000099523,
  "MEAN_MOTION_DOT": 0.00001897,
  "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-001
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/61047

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