▸Orbital parameters

Orbit class	LEO
Inclination	52.9753°
Eccentricity	0.0006454
Period	94.7 min
Apogee	508 km
Perigee	499 km
Mean motion	15.20857755 rev/day
RAAN	220.0040°
Arg of perigee	165.9423°
Mean anomaly	194.1752°
B*	2.0708e-4
Rev at epoch	10,071

▸Two-line element set (TLE)

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

1 61048U 24163D 26187.57009699 .00004308 00000-0 20708-3 0 9999

2 61048 52.9753 220.0040 0006454 165.9423 194.1752 15.20857755100712

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPACEMOBILE-002",
  "OBJECT_ID": "2024-163D",
  "EPOCH": "2026-07-06T13:40:56.38+00:00",
  "MEAN_MOTION": 15.20857755,
  "ECCENTRICITY": 0.0006454,
  "INCLINATION": 52.9753,
  "RA_OF_ASC_NODE": 220.004,
  "ARG_OF_PERICENTER": 165.9423,
  "MEAN_ANOMALY": 194.1752,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61048,
  "REV_AT_EPOCH": 10071,
  "BSTAR": 0.00020708,
  "MEAN_MOTION_DOT": 0.00004308,
  "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-002
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/61048

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