▸Orbital parameters

Orbit class	LEO
Inclination	88.9722°
Eccentricity	0.0017401
Period	106.6 min
Apogee	1,082 km
Perigee	1,056 km
Mean motion	13.51015462 rev/day
RAAN	81.6985°
Arg of perigee	96.3543°
Mean anomaly	263.9591°
B*	1.3223e-4
Rev at epoch	7,510

▸Two-line element set (TLE)

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

1 62800U 25016R 26188.12834498 .00000098 00000-0 13223-3 0 9995

2 62800 88.9722 81.6985 0017401 96.3543 263.9591 13.51015462 75100

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-70",
  "OBJECT_ID": "2025-016R",
  "EPOCH": "2026-07-07T03:04:49.006+00:00",
  "MEAN_MOTION": 13.51015462,
  "ECCENTRICITY": 0.0017401,
  "INCLINATION": 88.9722,
  "RA_OF_ASC_NODE": 81.6985,
  "ARG_OF_PERICENTER": 96.3543,
  "MEAN_ANOMALY": 263.9591,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62800,
  "REV_AT_EPOCH": 7510,
  "BSTAR": 0.00013223,
  "MEAN_MOTION_DOT": 9.8e-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-70
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/62800

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