▸Orbital parameters

Orbit class	LEO
Inclination	88.9723°
Eccentricity	0.0014133
Period	106.6 min
Apogee	1,079 km
Perigee	1,058 km
Mean motion	13.51042316 rev/day
RAAN	298.6337°
Arg of perigee	242.7437°
Mean anomaly	117.2274°
B*	2.3024e-4
Rev at epoch	7,527

▸Two-line element set (TLE)

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

1 63170U 25046M 26188.18860198 .00000161 00000-0 23024-3 0 9992

2 63170 88.9723 298.6337 0014133 242.7437 117.2274 13.51042316 75276

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-84",
  "OBJECT_ID": "2025-046M",
  "EPOCH": "2026-07-07T04:31:35.211+00:00",
  "MEAN_MOTION": 13.51042316,
  "ECCENTRICITY": 0.0014133,
  "INCLINATION": 88.9723,
  "RA_OF_ASC_NODE": 298.6337,
  "ARG_OF_PERICENTER": 242.7437,
  "MEAN_ANOMALY": 117.2274,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63170,
  "REV_AT_EPOCH": 7527,
  "BSTAR": 0.00023024,
  "MEAN_MOTION_DOT": 0.00000161,
  "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-84
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/63170

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