▸Orbital parameters

Orbit class	LEO
Inclination	88.9726°
Eccentricity	0.0013004
Period	106.6 min
Apogee	1,078 km
Perigee	1,059 km
Mean motion	13.51017497 rev/day
RAAN	298.6939°
Arg of perigee	245.7757°
Mean anomaly	114.2035°
B*	2.0895e-4
Rev at epoch	7,524

▸Two-line element set (TLE)

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

1 63165U 25046G 26188.13066624 .00000147 00000-0 20895-3 0 9990

2 63165 88.9726 298.6939 0013004 245.7757 114.2035 13.51017497 75246

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-79",
  "OBJECT_ID": "2025-046G",
  "EPOCH": "2026-07-07T03:08:09.563+00:00",
  "MEAN_MOTION": 13.51017497,
  "ECCENTRICITY": 0.0013004,
  "INCLINATION": 88.9726,
  "RA_OF_ASC_NODE": 298.6939,
  "ARG_OF_PERICENTER": 245.7757,
  "MEAN_ANOMALY": 114.2035,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63165,
  "REV_AT_EPOCH": 7524,
  "BSTAR": 0.00020895,
  "MEAN_MOTION_DOT": 0.00000147,
  "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-79
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/63165

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