▸Orbital parameters

Orbit class	LEO
Inclination	88.9723°
Eccentricity	0.0014951
Period	106.6 min
Apogee	1,080 km
Perigee	1,057 km
Mean motion	13.51022261 rev/day
RAAN	298.6280°
Arg of perigee	243.6683°
Mean anomaly	116.2933°
B*	2.1645e-4
Rev at epoch	7,527

▸Two-line element set (TLE)

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

1 63175U 25046S 26188.14296735 .00000152 00000-0 21645-3 0 9990

2 63175 88.9723 298.6280 0014951 243.6683 116.2933 13.51022261 75277

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-89",
  "OBJECT_ID": "2025-046S",
  "EPOCH": "2026-07-07T03:25:52.379+00:00",
  "MEAN_MOTION": 13.51022261,
  "ECCENTRICITY": 0.0014951,
  "INCLINATION": 88.9723,
  "RA_OF_ASC_NODE": 298.628,
  "ARG_OF_PERICENTER": 243.6683,
  "MEAN_ANOMALY": 116.2933,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63175,
  "REV_AT_EPOCH": 7527,
  "BSTAR": 0.00021645,
  "MEAN_MOTION_DOT": 0.00000152,
  "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-89
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/63175

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