▸Orbital parameters

Orbit class	LEO
Inclination	89.0094°
Eccentricity	0.0018605
Period	104.9 min
Apogee	1,005 km
Perigee	978 km
Mean motion	13.72261606 rev/day
RAAN	20.1013°
Arg of perigee	47.3758°
Mean anomaly	312.8970°
B*	-2.3730e+0
Rev at epoch	708

▸Two-line element set (TLE)

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

1 69107U 26108D 26188.01605948 -.02022689 00000-0 -23730+1 0 9994

2 69107 89.0094 20.1013 0018605 47.3758 312.8970 13.72261606 7085

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-148",
  "OBJECT_ID": "2026-108D",
  "EPOCH": "2026-07-07T00:23:07.539+00:00",
  "MEAN_MOTION": 13.72261606,
  "ECCENTRICITY": 0.0018605,
  "INCLINATION": 89.0094,
  "RA_OF_ASC_NODE": 20.1013,
  "ARG_OF_PERICENTER": 47.3758,
  "MEAN_ANOMALY": 312.897,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69107,
  "REV_AT_EPOCH": 708,
  "BSTAR": -2.373,
  "MEAN_MOTION_DOT": -0.02022689,
  "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-148
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/69107

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