▸Orbital parameters

Orbit class	LEO
Inclination	88.9990°
Eccentricity	0.0002046
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51015926 rev/day
RAAN	40.6584°
Arg of perigee	92.9432°
Mean anomaly	267.1953°
B*	9.4313e-5
Rev at epoch	3,615

▸Two-line element set (TLE)

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

1 66037U 25233E 26187.99435338 .00000073 00000-0 94313-4 0 9999

2 66037 88.9990 40.6584 0002046 92.9432 267.1953 13.51015926 36156

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-95",
  "OBJECT_ID": "2025-233E",
  "EPOCH": "2026-07-06T23:51:52.132+00:00",
  "MEAN_MOTION": 13.51015926,
  "ECCENTRICITY": 0.0002046,
  "INCLINATION": 88.999,
  "RA_OF_ASC_NODE": 40.6584,
  "ARG_OF_PERICENTER": 92.9432,
  "MEAN_ANOMALY": 267.1953,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66037,
  "REV_AT_EPOCH": 3615,
  "BSTAR": 0.000094313,
  "MEAN_MOTION_DOT": 7.3e-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-95
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/66037

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