▸Orbital parameters

Orbit class	LEO
Inclination	49.9882°
Eccentricity	0.0012827
Period	97.0 min
Apogee	625 km
Perigee	607 km
Mean motion	14.84216278 rev/day
RAAN	308.9959°
Arg of perigee	27.2827°
Mean anomaly	332.8782°
B*	2.2227e-4
Rev at epoch	4,468

▸Two-line element set (TLE)

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

1 65556U 25201G 26187.61845808 .00001652 00000-0 22227-3 0 9993

2 65556 49.9882 308.9959 0012827 27.2827 332.8782 14.84216278 44688

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 07",
  "OBJECT_ID": "2025-201G",
  "EPOCH": "2026-07-06T14:50:34.778+00:00",
  "MEAN_MOTION": 14.84216278,
  "ECCENTRICITY": 0.0012827,
  "INCLINATION": 49.9882,
  "RA_OF_ASC_NODE": 308.9959,
  "ARG_OF_PERICENTER": 27.2827,
  "MEAN_ANOMALY": 332.8782,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65556,
  "REV_AT_EPOCH": 4468,
  "BSTAR": 0.00022227,
  "MEAN_MOTION_DOT": 0.00001652,
  "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 07
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/65556

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