▸Orbital parameters

Orbit class	LEO
Inclination	88.9803°
Eccentricity	0.0008689
Period	103.9 min
Apogee	948 km
Perigee	935 km
Mean motion	13.86404542 rev/day
RAAN	56.6344°
Arg of perigee	84.5254°
Mean anomaly	275.6908°
B*	1.7422e-4
Rev at epoch	9,753

▸Two-line element set (TLE)

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

1 61555U 24185D 26188.14145881 .00000215 00000-0 17422-3 0 9996

2 61555 88.9803 56.6344 0008689 84.5254 275.6908 13.86404542 97535

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-22",
  "OBJECT_ID": "2024-185D",
  "EPOCH": "2026-07-07T03:23:42.041+00:00",
  "MEAN_MOTION": 13.86404542,
  "ECCENTRICITY": 0.0008689,
  "INCLINATION": 88.9803,
  "RA_OF_ASC_NODE": 56.6344,
  "ARG_OF_PERICENTER": 84.5254,
  "MEAN_ANOMALY": 275.6908,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61555,
  "REV_AT_EPOCH": 9753,
  "BSTAR": 0.00017422,
  "MEAN_MOTION_DOT": 0.00000215,
  "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-22
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/61555

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