▸Orbital parameters

Orbit class	GEO
Inclination	0.8816°
Eccentricity	0.0000859
Period	1436.1 min
Apogee	35,790 km
Perigee	35,783 km
Mean motion	1.00273260 rev/day
RAAN	85.0783°
Arg of perigee	78.6909°
Mean anomaly	244.9048°
B*	0.0000e+0
Rev at epoch	3,491

▸Two-line element set (TLE)

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

1 41911U 17001A 26188.15823462 .00000008 00000-0 00000-0 0 9999

2 41911 0.8816 85.0783 0000859 78.6909 244.9048 1.00273260 34912

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TJS-2",
  "OBJECT_ID": "2017-001A",
  "EPOCH": "2026-07-07T03:47:51.471+00:00",
  "MEAN_MOTION": 1.0027326,
  "ECCENTRICITY": 0.0000859,
  "INCLINATION": 0.8816,
  "RA_OF_ASC_NODE": 85.0783,
  "ARG_OF_PERICENTER": 78.6909,
  "MEAN_ANOMALY": 244.9048,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41911,
  "REV_AT_EPOCH": 3491,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 8e-8,
  "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-2
Operator	China Aerospace CorpHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 5, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4000HIGHvia 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/41911

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