▸Orbital parameters

Orbit class	LEO
Inclination	89.0003°
Eccentricity	0.0001894
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51042808 rev/day
RAAN	41.1557°
Arg of perigee	89.7470°
Mean anomaly	270.3898°
B*	7.3714e-5
Rev at epoch	3,586

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 66042U 25233K 26187.63640978 .00000060 00000-0 73714-4 0 9992

2 66042 89.0003 41.1557 0001894 89.7470 270.3898 13.51042808 35861

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-100",
  "OBJECT_ID": "2025-233K",
  "EPOCH": "2026-07-06T15:16:25.805+00:00",
  "MEAN_MOTION": 13.51042808,
  "ECCENTRICITY": 0.0001894,
  "INCLINATION": 89.0003,
  "RA_OF_ASC_NODE": 41.1557,
  "ARG_OF_PERICENTER": 89.747,
  "MEAN_ANOMALY": 270.3898,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66042,
  "REV_AT_EPOCH": 3586,
  "BSTAR": 0.000073714,
  "MEAN_MOTION_DOT": 6e-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-100
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 17, 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/66042

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