▸Orbital parameters

Orbit class	LEO
Inclination	88.9780°
Eccentricity	0.0006878
Period	106.2 min
Apogee	1,057 km
Perigee	1,047 km
Mean motion	13.55638766 rev/day
RAAN	59.5401°
Arg of perigee	146.6368°
Mean anomaly	213.5220°
B*	7.1293e-5
Rev at epoch	9,588

▸Two-line element set (TLE)

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

1 61569U 24185T 26188.11788774 .00000062 00000-0 71293-4 0 9999

2 61569 88.9780 59.5401 0006878 146.6368 213.5220 13.55638766 95881

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-36",
  "OBJECT_ID": "2024-185T",
  "EPOCH": "2026-07-07T02:49:45.501+00:00",
  "MEAN_MOTION": 13.55638766,
  "ECCENTRICITY": 0.0006878,
  "INCLINATION": 88.978,
  "RA_OF_ASC_NODE": 59.5401,
  "ARG_OF_PERICENTER": 146.6368,
  "MEAN_ANOMALY": 213.522,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61569,
  "REV_AT_EPOCH": 9588,
  "BSTAR": 0.000071293,
  "MEAN_MOTION_DOT": 6.2e-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-36
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/61569

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