▸Orbital parameters

Orbit class	LEO
Inclination	89.0066°
Eccentricity	0.0013986
Period	106.6 min
Apogee	1,079 km
Perigee	1,058 km
Mean motion	13.51013141 rev/day
RAAN	20.3652°
Arg of perigee	322.4204°
Mean anomaly	37.5969°
B*	4.5468e-5
Rev at epoch	9,581

▸Two-line element set (TLE)

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

1 62253U 24232S 26188.14337939 .00000041 00000-0 45468-4 0 9991

2 62253 89.0066 20.3652 0013986 322.4204 37.5969 13.51013141 95813

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-52",
  "OBJECT_ID": "2024-232S",
  "EPOCH": "2026-07-07T03:26:27.979+00:00",
  "MEAN_MOTION": 13.51013141,
  "ECCENTRICITY": 0.0013986,
  "INCLINATION": 89.0066,
  "RA_OF_ASC_NODE": 20.3652,
  "ARG_OF_PERICENTER": 322.4204,
  "MEAN_ANOMALY": 37.5969,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62253,
  "REV_AT_EPOCH": 9581,
  "BSTAR": 0.000045468,
  "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-52
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/62253

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