▸Orbital parameters

Orbit class	LEO
Inclination	49.9827°
Eccentricity	0.0007360
Period	97.0 min
Apogee	621 km
Perigee	611 km
Mean motion	14.84228450 rev/day
RAAN	308.7300°
Arg of perigee	359.5225°
Mean anomaly	0.5705°
B*	2.2418e-4
Rev at epoch	4,468

▸Two-line element set (TLE)

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

1 65559U 25201K 26187.60349692 .00001669 00000-0 22418-3 0 9995

2 65559 49.9827 308.7300 0007360 359.5225 0.5705 14.84228450 44686

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 10",
  "OBJECT_ID": "2025-201K",
  "EPOCH": "2026-07-06T14:29:02.134+00:00",
  "MEAN_MOTION": 14.8422845,
  "ECCENTRICITY": 0.000736,
  "INCLINATION": 49.9827,
  "RA_OF_ASC_NODE": 308.73,
  "ARG_OF_PERICENTER": 359.5225,
  "MEAN_ANOMALY": 0.5705,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65559,
  "REV_AT_EPOCH": 4468,
  "BSTAR": 0.00022418,
  "MEAN_MOTION_DOT": 0.00001669,
  "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 10
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/65559

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