▸Orbital parameters

Orbit class	LEO
Inclination	88.9879°
Eccentricity	0.0012137
Period	105.2 min
Apogee	1,011 km
Perigee	993 km
Mean motion	13.69406217 rev/day
RAAN	339.4344°
Arg of perigee	40.5514°
Mean anomaly	319.6550°
B*	-2.4590e+0
Rev at epoch	784

▸Two-line element set (TLE)

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

1 69088U 26104R 26188.07712830 -.02000208 00000-0 -24590+1 0 9991

2 69088 88.9879 339.4344 0012137 40.5514 319.6550 13.69406217 7842

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-142",
  "OBJECT_ID": "2026-104R",
  "EPOCH": "2026-07-07T01:51:03.885+00:00",
  "MEAN_MOTION": 13.69406217,
  "ECCENTRICITY": 0.0012137,
  "INCLINATION": 88.9879,
  "RA_OF_ASC_NODE": 339.4344,
  "ARG_OF_PERICENTER": 40.5514,
  "MEAN_ANOMALY": 319.655,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69088,
  "REV_AT_EPOCH": 784,
  "BSTAR": -2.459,
  "MEAN_MOTION_DOT": -0.02000208,
  "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-142
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/69088

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