▸Orbital parameters

Orbit class	LEO
Inclination	88.9706°
Eccentricity	0.0017656
Period	106.6 min
Apogee	1,082 km
Perigee	1,055 km
Mean motion	13.51004775 rev/day
RAAN	81.6331°
Arg of perigee	103.5804°
Mean anomaly	256.7315°
B*	1.3994e-4
Rev at epoch	7,509

▸Two-line element set (TLE)

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

1 62790U 25016F 26188.12021169 .00000103 00000-0 13994-3 0 9998

2 62790 88.9706 81.6331 0017656 103.5804 256.7315 13.51004775 75095

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-60",
  "OBJECT_ID": "2025-016F",
  "EPOCH": "2026-07-07T02:53:06.29+00:00",
  "MEAN_MOTION": 13.51004775,
  "ECCENTRICITY": 0.0017656,
  "INCLINATION": 88.9706,
  "RA_OF_ASC_NODE": 81.6331,
  "ARG_OF_PERICENTER": 103.5804,
  "MEAN_ANOMALY": 256.7315,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62790,
  "REV_AT_EPOCH": 7509,
  "BSTAR": 0.00013994,
  "MEAN_MOTION_DOT": 0.00000103,
  "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-60
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/62790

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