▸Orbital parameters

Orbit class	SSO
Inclination	97.3858°
Eccentricity	0.0008440
Period	94.0 min
Apogee	474 km
Perigee	463 km
Mean motion	15.32538136 rev/day
RAAN	82.9188°
Arg of perigee	84.5451°
Mean anomaly	275.6754°
B*	3.8581e-4
Rev at epoch	7,307

▸Two-line element set (TLE)

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

1 63240U 25052AG 26188.15969506 .00012062 00000-0 38581-3 0 9994

2 63240 97.3858 82.9188 0008440 84.5451 275.6754 15.32538136 73076

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AL MUNTHER",
  "OBJECT_ID": "2025-052AG",
  "EPOCH": "2026-07-07T03:49:57.653+00:00",
  "MEAN_MOTION": 15.32538136,
  "ECCENTRICITY": 0.000844,
  "INCLINATION": 97.3858,
  "RA_OF_ASC_NODE": 82.9188,
  "ARG_OF_PERICENTER": 84.5451,
  "MEAN_ANOMALY": 275.6754,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63240,
  "REV_AT_EPOCH": 7307,
  "BSTAR": 0.00038581,
  "MEAN_MOTION_DOT": 0.00012062,
  "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	AL MUNTHER
Operator	National Space Science AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	BH
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/63240

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