▸Orbital parameters

Orbit class	LEO
Inclination	88.9723°
Eccentricity	0.0011750
Period	106.6 min
Apogee	1,077 km
Perigee	1,060 km
Mean motion	13.51014711 rev/day
RAAN	298.3936°
Arg of perigee	250.3034°
Mean anomaly	109.6850°
B*	2.2326e-4
Rev at epoch	7,540

▸Two-line element set (TLE)

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

1 63166U 25046H 26188.14720064 .00000156 00000-0 22326-3 0 9998

2 63166 88.9723 298.3936 0011750 250.3034 109.6850 13.51014711 75401

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-80",
  "OBJECT_ID": "2025-046H",
  "EPOCH": "2026-07-07T03:31:58.135+00:00",
  "MEAN_MOTION": 13.51014711,
  "ECCENTRICITY": 0.001175,
  "INCLINATION": 88.9723,
  "RA_OF_ASC_NODE": 298.3936,
  "ARG_OF_PERICENTER": 250.3034,
  "MEAN_ANOMALY": 109.685,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63166,
  "REV_AT_EPOCH": 7540,
  "BSTAR": 0.00022326,
  "MEAN_MOTION_DOT": 0.00000156,
  "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-80
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 11, 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/63166

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