▸Orbital parameters

Orbit class	LEO
Inclination	88.9879°
Eccentricity	0.0006691
Period	105.6 min
Apogee	1,029 km
Perigee	1,019 km
Mean motion	13.63245969 rev/day
RAAN	339.4643°
Arg of perigee	52.5020°
Mean anomaly	307.6746°
B*	-2.8396e+0
Rev at epoch	782

▸Two-line element set (TLE)

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

1 69085U 26104N 26188.03059213 -.02083684 00000-0 -28396+1 0 9990

2 69085 88.9879 339.4643 0006691 52.5020 307.6746 13.63245969 7825

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-139",
  "OBJECT_ID": "2026-104N",
  "EPOCH": "2026-07-07T00:44:03.16+00:00",
  "MEAN_MOTION": 13.63245969,
  "ECCENTRICITY": 0.0006691,
  "INCLINATION": 88.9879,
  "RA_OF_ASC_NODE": 339.4643,
  "ARG_OF_PERICENTER": 52.502,
  "MEAN_ANOMALY": 307.6746,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69085,
  "REV_AT_EPOCH": 782,
  "BSTAR": -2.8396,
  "MEAN_MOTION_DOT": -0.02083684,
  "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-139
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 12, 2026HIGHvia 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/69085

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