▸Orbital parameters

Orbit class	LEO
Inclination	88.9910°
Eccentricity	0.0002023
Period	106.6 min
Apogee	1,070 km
Perigee	1,067 km
Mean motion	13.51013291 rev/day
RAAN	318.9736°
Arg of perigee	116.3196°
Mean anomaly	243.8163°
B*	1.4325e-4
Rev at epoch	1,248

▸Two-line element set (TLE)

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

1 68636U 26075A 26188.14013442 .00000105 00000-0 14325-3 0 9997

2 68636 88.9910 318.9736 0002023 116.3196 243.8163 13.51013291 12485

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-109",
  "OBJECT_ID": "2026-075A",
  "EPOCH": "2026-07-07T03:21:47.614+00:00",
  "MEAN_MOTION": 13.51013291,
  "ECCENTRICITY": 0.0002023,
  "INCLINATION": 88.991,
  "RA_OF_ASC_NODE": 318.9736,
  "ARG_OF_PERICENTER": 116.3196,
  "MEAN_ANOMALY": 243.8163,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68636,
  "REV_AT_EPOCH": 1248,
  "BSTAR": 0.00014325,
  "MEAN_MOTION_DOT": 0.00000105,
  "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-109
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/68636

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