▸Orbital parameters

Orbit class	LEO
Inclination	88.9700°
Eccentricity	0.0017678
Period	106.6 min
Apogee	1,082 km
Perigee	1,055 km
Mean motion	13.51008271 rev/day
RAAN	81.5986°
Arg of perigee	110.3771°
Mean anomaly	249.9281°
B*	1.4855e-4
Rev at epoch	7,509

▸Two-line element set (TLE)

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

1 62786U 25016B 26188.05846219 .00000108 00000-0 14855-3 0 9998

2 62786 88.9700 81.5986 0017678 110.3771 249.9281 13.51008271 75093

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-56",
  "OBJECT_ID": "2025-016B",
  "EPOCH": "2026-07-07T01:24:11.133+00:00",
  "MEAN_MOTION": 13.51008271,
  "ECCENTRICITY": 0.0017678,
  "INCLINATION": 88.97,
  "RA_OF_ASC_NODE": 81.5986,
  "ARG_OF_PERICENTER": 110.3771,
  "MEAN_ANOMALY": 249.9281,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62786,
  "REV_AT_EPOCH": 7509,
  "BSTAR": 0.00014855,
  "MEAN_MOTION_DOT": 0.00000108,
  "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-56
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/62786

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