▸Orbital parameters

Orbit class	LEO
Inclination	88.9983°
Eccentricity	0.0005172
Period	102.4 min
Apogee	877 km
Perigee	869 km
Mean motion	14.06039575 rev/day
RAAN	359.7925°
Arg of perigee	123.2020°
Mean anomaly	236.9659°
B*	-1.3695e+0
Rev at epoch	462

▸Two-line element set (TLE)

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

1 69386U 26124E 26188.01895441 -.02079387 00000-0 -13695+1 0 9996

2 69386 88.9983 359.7925 0005172 123.2020 236.9659 14.06039575 4626

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-169",
  "OBJECT_ID": "2026-124E",
  "EPOCH": "2026-07-07T00:27:17.661+00:00",
  "MEAN_MOTION": 14.06039575,
  "ECCENTRICITY": 0.0005172,
  "INCLINATION": 88.9983,
  "RA_OF_ASC_NODE": 359.7925,
  "ARG_OF_PERICENTER": 123.202,
  "MEAN_ANOMALY": 236.9659,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69386,
  "REV_AT_EPOCH": 462,
  "BSTAR": -1.3695,
  "MEAN_MOTION_DOT": -0.02079387,
  "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-169
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 4, 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/69386

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