▸Orbital parameters

Orbit class	LEO
Inclination	49.9864°
Eccentricity	0.0007780
Period	97.0 min
Apogee	622 km
Perigee	611 km
Mean motion	14.84218273 rev/day
RAAN	310.3813°
Arg of perigee	39.8588°
Mean anomaly	320.2920°
B*	2.5638e-4
Rev at epoch	4,464

▸Two-line element set (TLE)

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

1 65551U 25201B 26187.37909002 .00001941 00000-0 25638-3 0 9998

2 65551 49.9864 310.3813 0007780 39.8588 320.2920 14.84218273 44642

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 02",
  "OBJECT_ID": "2025-201B",
  "EPOCH": "2026-07-06T09:05:53.378+00:00",
  "MEAN_MOTION": 14.84218273,
  "ECCENTRICITY": 0.00077803,
  "INCLINATION": 49.9864,
  "RA_OF_ASC_NODE": 310.3813,
  "ARG_OF_PERICENTER": 39.8588,
  "MEAN_ANOMALY": 320.292,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65551,
  "REV_AT_EPOCH": 4464,
  "BSTAR": 0.00025638019,
  "MEAN_MOTION_DOT": 0.00001941,
  "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	GEESAT-5 02
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 8, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	130HIGHvia 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/65551

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