▸Orbital parameters

Orbit class	LEO
Inclination	49.9920°
Eccentricity	0.0003180
Period	97.0 min
Apogee	618 km
Perigee	614 km
Mean motion	14.84206708 rev/day
RAAN	309.9367°
Arg of perigee	127.0745°
Mean anomaly	233.0484°
B*	2.3605e-4
Rev at epoch	4,467

▸Two-line element set (TLE)

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

1 65550U 25201A 26187.52112139 .00001769 00000-0 23605-3 0 9991

2 65550 49.9920 309.9367 0003180 127.0745 233.0484 14.84206708 44676

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 01",
  "OBJECT_ID": "2025-201A",
  "EPOCH": "2026-07-06T12:30:24.888+00:00",
  "MEAN_MOTION": 14.84206708,
  "ECCENTRICITY": 0.000318,
  "INCLINATION": 49.992,
  "RA_OF_ASC_NODE": 309.9367,
  "ARG_OF_PERICENTER": 127.0745,
  "MEAN_ANOMALY": 233.0484,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65550,
  "REV_AT_EPOCH": 4467,
  "BSTAR": 0.00023605,
  "MEAN_MOTION_DOT": 0.00001769,
  "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 01
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/65550

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