▸Orbital parameters

Orbit class	LEO
Inclination	89.0089°
Eccentricity	0.0020831
Period	104.5 min
Apogee	985 km
Perigee	955 km
Mean motion	13.78269838 rev/day
RAAN	20.0620°
Arg of perigee	51.2956°
Mean anomaly	309.0070°
B*	-2.1475e+0
Rev at epoch	711

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 69117U 26108P 26187.99060030 -.02022901 00000-0 -21475+1 0 9999

2 69117 89.0089 20.0620 0020831 51.2956 309.0070 13.78269838 7115

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-158",
  "OBJECT_ID": "2026-108P",
  "EPOCH": "2026-07-06T23:46:27.866+00:00",
  "MEAN_MOTION": 13.78269838,
  "ECCENTRICITY": 0.0020831,
  "INCLINATION": 89.0089,
  "RA_OF_ASC_NODE": 20.062,
  "ARG_OF_PERICENTER": 51.2956,
  "MEAN_ANOMALY": 309.007,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69117,
  "REV_AT_EPOCH": 711,
  "BSTAR": -2.1475,
  "MEAN_MOTION_DOT": -0.02022901,
  "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-158
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/69117

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