▸Orbital parameters

Orbit class	GEO
Inclination	0.7401°
Eccentricity	0.0001588
Period	1436.1 min
Apogee	35,793 km
Perigee	35,780 km
Mean motion	1.00272884 rev/day
RAAN	296.9908°
Arg of perigee	291.0841°
Mean anomaly	103.2328°
B*	0.0000e+0
Rev at epoch	547

▸Two-line element set (TLE)

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

1 62804U 25017A 26188.07743050 .00000131 00000-0 00000-0 0 9991

2 62804 0.7401 296.9908 0001588 291.0841 103.2328 1.00272884 5471

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TJS-14",
  "OBJECT_ID": "2025-017A",
  "EPOCH": "2026-07-07T01:51:29.995+00:00",
  "MEAN_MOTION": 1.00272884,
  "ECCENTRICITY": 0.0001588,
  "INCLINATION": 0.7401,
  "RA_OF_ASC_NODE": 296.9908,
  "ARG_OF_PERICENTER": 291.0841,
  "MEAN_ANOMALY": 103.2328,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62804,
  "REV_AT_EPOCH": 547,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000131,
  "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	TJS-14
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5000HIGHvia 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/62804

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