▸Orbital parameters

Orbit class	LEO
Inclination	88.9989°
Eccentricity	0.0002079
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51014806 rev/day
RAAN	41.1335°
Arg of perigee	87.9677°
Mean anomaly	272.1712°
B*	9.6760e-5
Rev at epoch	3,586

▸Two-line element set (TLE)

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

1 66044U 25233M 26187.65692803 .00000074 00000-0 96760-4 0 9991

2 66044 88.9989 41.1335 0002079 87.9677 272.1712 13.51014806 35865

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-102",
  "OBJECT_ID": "2025-233M",
  "EPOCH": "2026-07-06T15:45:58.582+00:00",
  "MEAN_MOTION": 13.51014806,
  "ECCENTRICITY": 0.0002079,
  "INCLINATION": 88.9989,
  "RA_OF_ASC_NODE": 41.1335,
  "ARG_OF_PERICENTER": 87.9677,
  "MEAN_ANOMALY": 272.1712,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66044,
  "REV_AT_EPOCH": 3586,
  "BSTAR": 0.00009676,
  "MEAN_MOTION_DOT": 7.4e-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-102
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/66044

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