▸Orbital parameters

Orbit class	LEO
Inclination	49.9913°
Eccentricity	0.0013497
Period	97.0 min
Apogee	625 km
Perigee	607 km
Mean motion	14.84230389 rev/day
RAAN	307.5761°
Arg of perigee	38.9587°
Mean anomaly	321.2321°
B*	1.9326e-4
Rev at epoch	4,472

▸Two-line element set (TLE)

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

1 65555U 25201F 26187.96281251 .00001407 00000-0 19326-3 0 9990

2 65555 49.9913 307.5761 0013497 38.9587 321.2321 14.84230389 44729

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 06",
  "OBJECT_ID": "2025-201F",
  "EPOCH": "2026-07-06T23:06:27.001+00:00",
  "MEAN_MOTION": 14.84230389,
  "ECCENTRICITY": 0.0013497,
  "INCLINATION": 49.9913,
  "RA_OF_ASC_NODE": 307.5761,
  "ARG_OF_PERICENTER": 38.9587,
  "MEAN_ANOMALY": 321.2321,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65555,
  "REV_AT_EPOCH": 4472,
  "BSTAR": 0.00019326,
  "MEAN_MOTION_DOT": 0.00001407,
  "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 06
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/65555

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