▸Orbital parameters

Orbit class	GEO
Inclination	0.0571°
Eccentricity	0.0000142
Period	1436.1 min
Apogee	35,787 km
Perigee	35,786 km
Mean motion	1.00272503 rev/day
RAAN	98.6088°
Arg of perigee	78.8542°
Mean anomaly	256.6230°
B*	0.0000e+0
Rev at epoch	42

▸Two-line element set (TLE)

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

1 69235U 26116A 26188.16291463 -.00000216 00000-0 00000-0 0 9998

2 69235 0.0571 98.6088 0000142 78.8542 256.6230 1.00272503 420

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TJS-24",
  "OBJECT_ID": "2026-116A",
  "EPOCH": "2026-07-07T03:54:35.824+00:00",
  "MEAN_MOTION": 1.00272503,
  "ECCENTRICITY": 0.0000142,
  "INCLINATION": 0.0571,
  "RA_OF_ASC_NODE": 98.6088,
  "ARG_OF_PERICENTER": 78.8542,
  "MEAN_ANOMALY": 256.623,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69235,
  "REV_AT_EPOCH": 42,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000216,
  "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-24
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 26, 2026HIGHvia 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/69235

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