▸Orbital parameters

Orbit class	LEO
Inclination	88.9752°
Eccentricity	0.0012446
Period	106.6 min
Apogee	1,078 km
Perigee	1,059 km
Mean motion	13.51020682 rev/day
RAAN	277.2926°
Arg of perigee	301.9181°
Mean anomaly	58.0759°
B*	1.4915e-4
Rev at epoch	9,533

▸Two-line element set (TLE)

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

1 60388U 24140K 26188.17681921 .00000108 00000-0 14915-3 0 9998

2 60388 88.9752 277.2926 0012446 301.9181 58.0759 13.51020682 95333

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-10",
  "OBJECT_ID": "2024-140K",
  "EPOCH": "2026-07-07T04:14:37.18+00:00",
  "MEAN_MOTION": 13.51020682,
  "ECCENTRICITY": 0.0012446,
  "INCLINATION": 88.9752,
  "RA_OF_ASC_NODE": 277.2926,
  "ARG_OF_PERICENTER": 301.9181,
  "MEAN_ANOMALY": 58.0759,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60388,
  "REV_AT_EPOCH": 9533,
  "BSTAR": 0.00014915,
  "MEAN_MOTION_DOT": 0.00000108,
  "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-10
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 6, 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/60388

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