▸Orbital parameters

Orbit class	LEO
Inclination	89.0057°
Eccentricity	0.0018214
Period	101.0 min
Apogee	820 km
Perigee	794 km
Mean motion	14.25530951 rev/day
RAAN	13.7915°
Arg of perigee	118.5957°
Mean anomaly	241.7071°
B*	4.3430e-5
Rev at epoch	13,079

▸Two-line element set (TLE)

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

1 62240U 24232D 26188.15531786 .00000118 00000-0 43430-4 0 9996

2 62240 89.0057 13.7915 0018214 118.5957 241.7071 14.25530951130790

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-39",
  "OBJECT_ID": "2024-232D",
  "EPOCH": "2026-07-07T03:43:39.463+00:00",
  "MEAN_MOTION": 14.25530951,
  "ECCENTRICITY": 0.0018214,
  "INCLINATION": 89.0057,
  "RA_OF_ASC_NODE": 13.7915,
  "ARG_OF_PERICENTER": 118.5957,
  "MEAN_ANOMALY": 241.7071,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62240,
  "REV_AT_EPOCH": 13079,
  "BSTAR": 0.00004343,
  "MEAN_MOTION_DOT": 0.00000118,
  "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-39
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 5, 2024HIGHvia 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/62240

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