▸Orbital parameters

Orbit class	LEO
Inclination	88.9725°
Eccentricity	0.0009243
Period	106.6 min
Apogee	1,075 km
Perigee	1,062 km
Mean motion	13.51021932 rev/day
RAAN	298.3780°
Arg of perigee	247.9339°
Mean anomaly	112.0831°
B*	2.2593e-4
Rev at epoch	7,541

▸Two-line element set (TLE)

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

1 63172U 25046P 26188.11832211 .00000158 00000-0 22593-3 0 9998

2 63172 88.9725 298.3780 0009243 247.9339 112.0831 13.51021932 75412

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-86",
  "OBJECT_ID": "2025-046P",
  "EPOCH": "2026-07-07T02:50:23.03+00:00",
  "MEAN_MOTION": 13.51021932,
  "ECCENTRICITY": 0.0009243,
  "INCLINATION": 88.9725,
  "RA_OF_ASC_NODE": 298.378,
  "ARG_OF_PERICENTER": 247.9339,
  "MEAN_ANOMALY": 112.0831,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63172,
  "REV_AT_EPOCH": 7541,
  "BSTAR": 0.00022593,
  "MEAN_MOTION_DOT": 0.00000158,
  "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-86
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/63172

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