▸Orbital parameters

Orbit class	LEO
Inclination	88.9909°
Eccentricity	0.0001947
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51015608 rev/day
RAAN	319.0289°
Arg of perigee	110.9595°
Mean anomaly	249.1765°
B*	1.3295e-4
Rev at epoch	1,239

▸Two-line element set (TLE)

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

1 68649U 26075P 26187.37889884 .00000098 00000-0 13295-3 0 9992

2 68649 88.9909 319.0289 0001947 110.9595 249.1765 13.51015608 12390

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-122",
  "OBJECT_ID": "2026-075P",
  "EPOCH": "2026-07-06T09:05:36.86+00:00",
  "MEAN_MOTION": 13.51015608,
  "ECCENTRICITY": 0.00019469,
  "INCLINATION": 88.9909,
  "RA_OF_ASC_NODE": 319.0289,
  "ARG_OF_PERICENTER": 110.9595,
  "MEAN_ANOMALY": 249.1765,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68649,
  "REV_AT_EPOCH": 1239,
  "BSTAR": 0.00013295022,
  "MEAN_MOTION_DOT": 9.8e-7,
  "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-122
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Apr 7, 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/68649

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