▸Orbital parameters

Orbit class	LEO
Inclination	49.9868°
Eccentricity	0.0008050
Period	97.0 min
Apogee	622 km
Perigee	610 km
Mean motion	14.84266836 rev/day
RAAN	310.0314°
Arg of perigee	343.4932°
Mean anomaly	16.5743°
B*	1.8413e-4
Rev at epoch	4,466

▸Two-line element set (TLE)

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

1 65553U 25201D 26187.56194509 .00001331 00000-0 18413-3 0 9995

2 65553 49.9868 310.0314 0008050 343.4932 16.5743 14.84266836 44667

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 04",
  "OBJECT_ID": "2025-201D",
  "EPOCH": "2026-07-06T13:29:12.056+00:00",
  "MEAN_MOTION": 14.84266836,
  "ECCENTRICITY": 0.000805,
  "INCLINATION": 49.9868,
  "RA_OF_ASC_NODE": 310.0314,
  "ARG_OF_PERICENTER": 343.4932,
  "MEAN_ANOMALY": 16.5743,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65553,
  "REV_AT_EPOCH": 4466,
  "BSTAR": 0.00018413,
  "MEAN_MOTION_DOT": 0.00001331,
  "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 04
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/65553

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