▸Orbital parameters

Orbit class	LEO
Inclination	88.9886°
Eccentricity	0.0010885
Period	105.5 min
Apogee	1,026 km
Perigee	1,010 km
Mean motion	13.64826064 rev/day
RAAN	339.4459°
Arg of perigee	39.1729°
Mean anomaly	321.0216°
B*	-2.8353e+0
Rev at epoch	783

▸Two-line element set (TLE)

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

1 69090U 26104T 26188.03233529 -.02131416 00000-0 -28353+1 0 9990

2 69090 88.9886 339.4459 0010885 39.1729 321.0216 13.64826064 7836

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-144",
  "OBJECT_ID": "2026-104T",
  "EPOCH": "2026-07-07T00:46:33.769+00:00",
  "MEAN_MOTION": 13.64826064,
  "ECCENTRICITY": 0.0010885,
  "INCLINATION": 88.9886,
  "RA_OF_ASC_NODE": 339.4459,
  "ARG_OF_PERICENTER": 39.1729,
  "MEAN_ANOMALY": 321.0216,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69090,
  "REV_AT_EPOCH": 783,
  "BSTAR": -2.8353,
  "MEAN_MOTION_DOT": -0.02131416,
  "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-144
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/69090

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