▸Orbital parameters

Orbit class	LEO
Inclination	49.9869°
Eccentricity	0.0010586
Period	97.0 min
Apogee	624 km
Perigee	609 km
Mean motion	14.84205971 rev/day
RAAN	310.3550°
Arg of perigee	334.0215°
Mean anomaly	26.0191°
B*	2.5226e-4
Rev at epoch	4,464

▸Two-line element set (TLE)

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

1 65552U 25201C 26187.37141703 .00001906 00000-0 25226-3 0 9999

2 65552 49.9869 310.3550 0010586 334.0215 26.0191 14.84205971 44643

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 03",
  "OBJECT_ID": "2025-201C",
  "EPOCH": "2026-07-06T08:54:50.431+00:00",
  "MEAN_MOTION": 14.84205971,
  "ECCENTRICITY": 0.00105862,
  "INCLINATION": 49.9869,
  "RA_OF_ASC_NODE": 310.355,
  "ARG_OF_PERICENTER": 334.0215,
  "MEAN_ANOMALY": 26.0191,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65552,
  "REV_AT_EPOCH": 4464,
  "BSTAR": 0.00025225767,
  "MEAN_MOTION_DOT": 0.00001906,
  "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 03
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/65552

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