▸Orbital parameters

Orbit class	LEO
Inclination	88.9725°
Eccentricity	0.0013124
Period	105.7 min
Apogee	1,038 km
Perigee	1,019 km
Mean motion	13.62048624 rev/day
RAAN	297.8764°
Arg of perigee	217.1380°
Mean anomaly	142.8870°
B*	2.1346e-4
Rev at epoch	7,569

▸Two-line element set (TLE)

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

1 63169U 25046L 26188.13416377 .00000177 00000-0 21346-3 0 9993

2 63169 88.9725 297.8764 0013124 217.1380 142.8870 13.62048624 75695

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-83",
  "OBJECT_ID": "2025-046L",
  "EPOCH": "2026-07-07T03:13:11.75+00:00",
  "MEAN_MOTION": 13.62048624,
  "ECCENTRICITY": 0.0013124,
  "INCLINATION": 88.9725,
  "RA_OF_ASC_NODE": 297.8764,
  "ARG_OF_PERICENTER": 217.138,
  "MEAN_ANOMALY": 142.887,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63169,
  "REV_AT_EPOCH": 7569,
  "BSTAR": 0.00021346,
  "MEAN_MOTION_DOT": 0.00000177,
  "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-83
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/63169

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