▸Orbital parameters

Orbit class	LEO
Inclination	88.9720°
Eccentricity	0.0017965
Period	106.6 min
Apogee	1,082 km
Perigee	1,055 km
Mean motion	13.51021747 rev/day
RAAN	81.6894°
Arg of perigee	103.3324°
Mean anomaly	256.9831°
B*	1.2525e-4
Rev at epoch	7,510

▸Two-line element set (TLE)

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

1 62792U 25016H 26188.15709845 .00000093 00000-0 12525-3 0 9994

2 62792 88.9720 81.6894 0017965 103.3324 256.9831 13.51021747 75100

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-62",
  "OBJECT_ID": "2025-016H",
  "EPOCH": "2026-07-07T03:46:13.306+00:00",
  "MEAN_MOTION": 13.51021747,
  "ECCENTRICITY": 0.0017965,
  "INCLINATION": 88.972,
  "RA_OF_ASC_NODE": 81.6894,
  "ARG_OF_PERICENTER": 103.3324,
  "MEAN_ANOMALY": 256.9831,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62792,
  "REV_AT_EPOCH": 7510,
  "BSTAR": 0.00012525,
  "MEAN_MOTION_DOT": 9.3e-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	QIANFAN-62
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	267HIGHvia 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/62792

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