▸Orbital parameters

Orbit class	LEO
Inclination	52.9667°
Eccentricity	0.0007073
Period	94.7 min
Apogee	508 km
Perigee	499 km
Mean motion	15.20801145 rev/day
RAAN	220.1743°
Arg of perigee	196.8401°
Mean anomaly	163.2360°
B*	5.1661e-4
Rev at epoch	10,070

▸Two-line element set (TLE)

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

1 61049U 24163E 26187.48682537 .00011231 00000-0 51661-3 0 9993

2 61049 52.9667 220.1743 0007073 196.8401 163.2360 15.20801145100708

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SPACEMOBILE-004",
  "OBJECT_ID": "2024-163E",
  "EPOCH": "2026-07-06T11:41:01.712+00:00",
  "MEAN_MOTION": 15.20801145,
  "ECCENTRICITY": 0.0007073,
  "INCLINATION": 52.9667,
  "RA_OF_ASC_NODE": 220.1743,
  "ARG_OF_PERICENTER": 196.8401,
  "MEAN_ANOMALY": 163.236,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61049,
  "REV_AT_EPOCH": 10070,
  "BSTAR": 0.00051661,
  "MEAN_MOTION_DOT": 0.00011231,
  "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-004
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/61049

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