▸Orbital parameters

Orbit class	LEO
Inclination	49.9813°
Eccentricity	0.0010725
Period	97.0 min
Apogee	624 km
Perigee	609 km
Mean motion	14.84225087 rev/day
RAAN	309.2225°
Arg of perigee	352.8988°
Mean anomaly	7.1796°
B*	2.1841e-4
Rev at epoch	4,467

▸Two-line element set (TLE)

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

1 65554U 25201E 26187.56629406 .00001620 00000-0 21841-3 0 9995

2 65554 49.9813 309.2225 0010725 352.8988 7.1796 14.84225087 44674

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 05",
  "OBJECT_ID": "2025-201E",
  "EPOCH": "2026-07-06T13:35:27.807+00:00",
  "MEAN_MOTION": 14.84225087,
  "ECCENTRICITY": 0.0010725,
  "INCLINATION": 49.9813,
  "RA_OF_ASC_NODE": 309.2225,
  "ARG_OF_PERICENTER": 352.8988,
  "MEAN_ANOMALY": 7.1796,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65554,
  "REV_AT_EPOCH": 4467,
  "BSTAR": 0.00021841,
  "MEAN_MOTION_DOT": 0.0000162,
  "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 05
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/65554

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