▸Orbital parameters

Orbit class	LEO
Inclination	49.9985°
Eccentricity	0.0016656
Period	97.0 min
Apogee	627 km
Perigee	604 km
Mean motion	14.84297307 rev/day
RAAN	350.9562°
Arg of perigee	154.5242°
Mean anomaly	205.6520°
B*	2.4684e-4
Rev at epoch	9,972

▸Two-line element set (TLE)

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

1 61016U 24159F 26188.10600440 .00001866 00000-0 24684-3 0 9993

2 61016 49.9985 350.9562 0016656 154.5242 205.6520 14.84297307 99729

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 06",
  "OBJECT_ID": "2024-159F",
  "EPOCH": "2026-07-07T02:32:38.78+00:00",
  "MEAN_MOTION": 14.84297307,
  "ECCENTRICITY": 0.0016656,
  "INCLINATION": 49.9985,
  "RA_OF_ASC_NODE": 350.9562,
  "ARG_OF_PERICENTER": 154.5242,
  "MEAN_ANOMALY": 205.652,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61016,
  "REV_AT_EPOCH": 9972,
  "BSTAR": 0.00024684,
  "MEAN_MOTION_DOT": 0.00001866,
  "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-3 06
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 5, 2024HIGHvia 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/61016

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