▸Orbital parameters

Orbit class	LEO
Inclination	88.9844°
Eccentricity	0.0009249
Period	106.6 min
Apogee	1,076 km
Perigee	1,063 km
Mean motion	13.50790238 rev/day
RAAN	59.7791°
Arg of perigee	178.0776°
Mean anomaly	182.0412°
B*	1.6491e-4
Rev at epoch	9,590

▸Two-line element set (TLE)

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

1 61565U 24185P 26188.13217178 .00000118 00000-0 16491-3 0 9992

2 61565 88.9844 59.7791 0009249 178.0776 182.0412 13.50790238 95903

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-32",
  "OBJECT_ID": "2024-185P",
  "EPOCH": "2026-07-07T03:10:19.642+00:00",
  "MEAN_MOTION": 13.50790238,
  "ECCENTRICITY": 0.0009249,
  "INCLINATION": 88.9844,
  "RA_OF_ASC_NODE": 59.7791,
  "ARG_OF_PERICENTER": 178.0776,
  "MEAN_ANOMALY": 182.0412,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61565,
  "REV_AT_EPOCH": 9590,
  "BSTAR": 0.00016491,
  "MEAN_MOTION_DOT": 0.00000118,
  "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-32
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/61565

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