▸Orbital parameters

Orbit class	LEO
Inclination	89.0099°
Eccentricity	0.0012589
Period	106.6 min
Apogee	1,078 km
Perigee	1,059 km
Mean motion	13.51009035 rev/day
RAAN	20.1493°
Arg of perigee	335.0731°
Mean anomaly	24.9811°
B*	2.8486e-5
Rev at epoch	12,746

▸Two-line element set (TLE)

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

1 62241U 24232E 26188.16811431 .00000030 00000-0 28486-4 0 9993

2 62241 89.0099 20.1493 0012589 335.0731 24.9811 13.51009035127460

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-40",
  "OBJECT_ID": "2024-232E",
  "EPOCH": "2026-07-07T04:02:05.076+00:00",
  "MEAN_MOTION": 13.51009035,
  "ECCENTRICITY": 0.0012589,
  "INCLINATION": 89.0099,
  "RA_OF_ASC_NODE": 20.1493,
  "ARG_OF_PERICENTER": 335.0731,
  "MEAN_ANOMALY": 24.9811,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62241,
  "REV_AT_EPOCH": 12746,
  "BSTAR": 0.000028486,
  "MEAN_MOTION_DOT": 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-40
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/62241

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