▸Orbital parameters

Orbit class	LEO
Inclination	63.4029°
Eccentricity	0.0068904
Period	107.0 min
Apogee	1,141 km
Perigee	1,038 km
Mean motion	13.45392842 rev/day
RAAN	47.0638°
Arg of perigee	355.6026°
Mean anomaly	4.4386°
B*	3.0805e-5
Rev at epoch	16,062

▸Two-line element set (TLE)

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

1 56157U 23048A 26188.15610954 -.00000072 00000-0 30805-4 0 9997

2 56157 63.4029 47.0638 0068904 355.6026 4.4386 13.45392842160623

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2023-048A",
  "OBJECT_ID": "2023-048A",
  "EPOCH": "2026-07-07T03:44:47.864+00:00",
  "MEAN_MOTION": 13.45392842,
  "ECCENTRICITY": 0.0068904,
  "INCLINATION": 63.4029,
  "RA_OF_ASC_NODE": 47.0638,
  "ARG_OF_PERICENTER": 355.6026,
  "MEAN_ANOMALY": 4.4386,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56157,
  "REV_AT_EPOCH": 16062,
  "BSTAR": 0.000030805,
  "MEAN_MOTION_DOT": -7.2e-7,
  "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	2023-048A
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 31, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/56157

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