▸Orbital parameters

Orbit class	LEO
Inclination	88.9876°
Eccentricity	0.0004838
Period	105.8 min
Apogee	1,033 km
Perigee	1,026 km
Mean motion	13.61667892 rev/day
RAAN	339.4778°
Arg of perigee	58.2649°
Mean anomaly	301.8979°
B*	-2.8766e+0
Rev at epoch	781

▸Two-line element set (TLE)

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

1 69081U 26104J 26188.00362786 -.02059486 00000-0 -28766+1 0 9999

2 69081 88.9876 339.4778 0004838 58.2649 301.8979 13.61667892 7812

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-135",
  "OBJECT_ID": "2026-104J",
  "EPOCH": "2026-07-07T00:05:13.447+00:00",
  "MEAN_MOTION": 13.61667892,
  "ECCENTRICITY": 0.0004838,
  "INCLINATION": 88.9876,
  "RA_OF_ASC_NODE": 339.4778,
  "ARG_OF_PERICENTER": 58.2649,
  "MEAN_ANOMALY": 301.8979,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69081,
  "REV_AT_EPOCH": 781,
  "BSTAR": -2.8766,
  "MEAN_MOTION_DOT": -0.02059486,
  "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-135
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/69081

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