▸Orbital parameters

Orbit class	LEO
Inclination	89.0100°
Eccentricity	0.0018756
Period	104.6 min
Apogee	990 km
Perigee	963 km
Mean motion	13.76451504 rev/day
RAAN	20.0863°
Arg of perigee	35.0939°
Mean anomaly	325.1458°
B*	-2.2613e+0
Rev at epoch	709

▸Two-line element set (TLE)

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

1 69109U 26108F 26188.02236183 -.02063026 00000-0 -22613+1 0 9997

2 69109 89.0100 20.0863 0018756 35.0939 325.1458 13.76451504 7090

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-150",
  "OBJECT_ID": "2026-108F",
  "EPOCH": "2026-07-07T00:32:12.062+00:00",
  "MEAN_MOTION": 13.76451504,
  "ECCENTRICITY": 0.0018756,
  "INCLINATION": 89.01,
  "RA_OF_ASC_NODE": 20.0863,
  "ARG_OF_PERICENTER": 35.0939,
  "MEAN_ANOMALY": 325.1458,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69109,
  "REV_AT_EPOCH": 709,
  "BSTAR": -2.2613,
  "MEAN_MOTION_DOT": -0.02063026,
  "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-150
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 17, 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/69109

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