▸Orbital parameters

Orbit class	LEO
Inclination	88.9988°
Eccentricity	0.0001914
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51014836 rev/day
RAAN	41.1989°
Arg of perigee	93.5321°
Mean anomaly	266.6049°
B*	8.1783e-5
Rev at epoch	3,585

▸Two-line element set (TLE)

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

1 66038U 25233F 26188.01904163 .00000065 00000-0 81783-4 0 9999

2 66038 88.9988 41.1989 0001914 93.5321 266.6049 13.51014836 35851

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-96",
  "OBJECT_ID": "2025-233F",
  "EPOCH": "2026-07-07T00:27:25.197+00:00",
  "MEAN_MOTION": 13.51014836,
  "ECCENTRICITY": 0.0001914,
  "INCLINATION": 88.9988,
  "RA_OF_ASC_NODE": 41.1989,
  "ARG_OF_PERICENTER": 93.5321,
  "MEAN_ANOMALY": 266.6049,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66038,
  "REV_AT_EPOCH": 3585,
  "BSTAR": 0.000081783,
  "MEAN_MOTION_DOT": 6.5e-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-96
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/66038

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