▸Orbital parameters

Orbit class	LEO
Inclination	89.0098°
Eccentricity	0.0021829
Period	105.1 min
Apogee	1,016 km
Perigee	983 km
Mean motion	13.70045551 rev/day
RAAN	20.1150°
Arg of perigee	52.1298°
Mean anomaly	308.1835°
B*	-2.5133e+0
Rev at epoch	708

▸Two-line element set (TLE)

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

1 69108U 26108E 26187.97019926 -.02063849 00000-0 -25133+1 0 9996

2 69108 89.0098 20.1150 0021829 52.1298 308.1835 13.70045551 7082

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-149",
  "OBJECT_ID": "2026-108E",
  "EPOCH": "2026-07-06T23:17:05.216+00:00",
  "MEAN_MOTION": 13.70045551,
  "ECCENTRICITY": 0.0021829,
  "INCLINATION": 89.0098,
  "RA_OF_ASC_NODE": 20.115,
  "ARG_OF_PERICENTER": 52.1298,
  "MEAN_ANOMALY": 308.1835,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69108,
  "REV_AT_EPOCH": 708,
  "BSTAR": -2.5133,
  "MEAN_MOTION_DOT": -0.02063849,
  "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-149
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/69108

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