▸Orbital parameters

Orbit class	LEO
Inclination	88.9741°
Eccentricity	0.0014492
Period	106.6 min
Apogee	1,079 km
Perigee	1,058 km
Mean motion	13.51019517 rev/day
RAAN	277.9244°
Arg of perigee	327.4616°
Mean anomaly	32.5640°
B*	1.4019e-4
Rev at epoch	9,520

▸Two-line element set (TLE)

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

1 60387U 24140J 26188.17269564 .00000103 00000-0 14019-3 0 9992

2 60387 88.9741 277.9244 0014492 327.4616 32.5640 13.51019517 95206

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-9",
  "OBJECT_ID": "2024-140J",
  "EPOCH": "2026-07-07T04:08:40.903+00:00",
  "MEAN_MOTION": 13.51019517,
  "ECCENTRICITY": 0.0014492,
  "INCLINATION": 88.9741,
  "RA_OF_ASC_NODE": 277.9244,
  "ARG_OF_PERICENTER": 327.4616,
  "MEAN_ANOMALY": 32.564,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60387,
  "REV_AT_EPOCH": 9520,
  "BSTAR": 0.00014019,
  "MEAN_MOTION_DOT": 0.00000103,
  "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-9
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/60387

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