▸Orbital parameters

Orbit class	LEO
Inclination	88.9810°
Eccentricity	0.0007759
Period	104.5 min
Apogee	977 km
Perigee	966 km
Mean motion	13.77921553 rev/day
RAAN	57.4748°
Arg of perigee	100.7869°
Mean anomaly	259.4172°
B*	1.7623e-4
Rev at epoch	9,709

▸Two-line element set (TLE)

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

1 61559U 24185H 26188.13474962 .00000190 00000-0 17623-3 0 9999

2 61559 88.9810 57.4748 0007759 100.7869 259.4172 13.77921553 97094

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-26",
  "OBJECT_ID": "2024-185H",
  "EPOCH": "2026-07-07T03:14:02.367+00:00",
  "MEAN_MOTION": 13.77921553,
  "ECCENTRICITY": 0.0007759,
  "INCLINATION": 88.981,
  "RA_OF_ASC_NODE": 57.4748,
  "ARG_OF_PERICENTER": 100.7869,
  "MEAN_ANOMALY": 259.4172,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61559,
  "REV_AT_EPOCH": 9709,
  "BSTAR": 0.00017623,
  "MEAN_MOTION_DOT": 0.0000019,
  "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-26
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 15, 2024HIGHvia 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/61559

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