▸Orbital parameters

Orbit class	LEO
Inclination	89.0068°
Eccentricity	0.0013678
Period	106.6 min
Apogee	1,079 km
Perigee	1,058 km
Mean motion	13.51010580 rev/day
RAAN	20.4846°
Arg of perigee	328.8940°
Mean anomaly	31.1400°
B*	4.4940e-5
Rev at epoch	12,710

▸Two-line element set (TLE)

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

1 62248U 24232M 26188.08172362 .00000041 00000-0 44940-4 0 9999

2 62248 89.0068 20.4846 0013678 328.8940 31.1400 13.51010580127102

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-47",
  "OBJECT_ID": "2024-232M",
  "EPOCH": "2026-07-07T01:57:40.921+00:00",
  "MEAN_MOTION": 13.5101058,
  "ECCENTRICITY": 0.0013678,
  "INCLINATION": 89.0068,
  "RA_OF_ASC_NODE": 20.4846,
  "ARG_OF_PERICENTER": 328.894,
  "MEAN_ANOMALY": 31.14,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62248,
  "REV_AT_EPOCH": 12710,
  "BSTAR": 0.00004494,
  "MEAN_MOTION_DOT": 4.1e-7,
  "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-47
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 5, 2024HIGHvia 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/62248

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