▸Orbital parameters

Orbit class	LEO
Inclination	88.9940°
Eccentricity	0.0020457
Period	102.1 min
Apogee	874 km
Perigee	845 km
Mean motion	14.10014634 rev/day
RAAN	278.1938°
Arg of perigee	90.9577°
Mean anomaly	269.3951°
B*	-1.2889e+0
Rev at epoch	451

▸Two-line element set (TLE)

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

1 69418U 26125T 26187.99615536 -.02104717 00000-0 -12889+1 0 9994

2 69418 88.9940 278.1938 0020457 90.9577 269.3951 14.10014634 4510

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-200",
  "OBJECT_ID": "2026-125T",
  "EPOCH": "2026-07-06T23:54:27.823+00:00",
  "MEAN_MOTION": 14.10014634,
  "ECCENTRICITY": 0.0020457,
  "INCLINATION": 88.994,
  "RA_OF_ASC_NODE": 278.1938,
  "ARG_OF_PERICENTER": 90.9577,
  "MEAN_ANOMALY": 269.3951,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69418,
  "REV_AT_EPOCH": 451,
  "BSTAR": -1.2889,
  "MEAN_MOTION_DOT": -0.02104717,
  "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-200
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 5, 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/69418

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