▸Orbital parameters

Orbit class	LEO
Inclination	89.0092°
Eccentricity	0.0019956
Period	104.5 min
Apogee	984 km
Perigee	954 km
Mean motion	13.78567817 rev/day
RAAN	20.0521°
Arg of perigee	51.4029°
Mean anomaly	308.8921°
B*	-2.1696e+0
Rev at epoch	711

▸Two-line element set (TLE)

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

1 69121U 26108T 26188.04157508 -.02051565 00000-0 -21696+1 0 9991

2 69121 89.0092 20.0521 0019956 51.4029 308.8921 13.78567817 7113

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-162",
  "OBJECT_ID": "2026-108T",
  "EPOCH": "2026-07-07T00:59:52.087+00:00",
  "MEAN_MOTION": 13.78567817,
  "ECCENTRICITY": 0.0019956,
  "INCLINATION": 89.0092,
  "RA_OF_ASC_NODE": 20.0521,
  "ARG_OF_PERICENTER": 51.4029,
  "MEAN_ANOMALY": 308.8921,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69121,
  "REV_AT_EPOCH": 711,
  "BSTAR": -2.1696,
  "MEAN_MOTION_DOT": -0.02051565,
  "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-162
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/69121

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