▸Orbital parameters

Orbit class	LEO
Inclination	89.0075°
Eccentricity	0.0018629
Period	104.7 min
Apogee	996 km
Perigee	968 km
Mean motion	13.74877852 rev/day
RAAN	20.0628°
Arg of perigee	32.6173°
Mean anomaly	327.6138°
B*	-2.3423e+0
Rev at epoch	711

▸Two-line element set (TLE)

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

1 69118U 26108Q 26188.02052522 -.02080598 00000-0 -23423+1 0 9993

2 69118 89.0075 20.0628 0018629 32.6173 327.6138 13.74877852 7113

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-159",
  "OBJECT_ID": "2026-108Q",
  "EPOCH": "2026-07-07T00:29:33.379+00:00",
  "MEAN_MOTION": 13.74877852,
  "ECCENTRICITY": 0.0018629,
  "INCLINATION": 89.0075,
  "RA_OF_ASC_NODE": 20.0628,
  "ARG_OF_PERICENTER": 32.6173,
  "MEAN_ANOMALY": 327.6138,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69118,
  "REV_AT_EPOCH": 711,
  "BSTAR": -2.3423,
  "MEAN_MOTION_DOT": -0.02080598,
  "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-159
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/69118

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