▸Orbital parameters

Orbit class	LEO
Inclination	88.9796°
Eccentricity	0.0009293
Period	101.1 min
Apogee	818 km
Perigee	805 km
Mean motion	14.24091418 rev/day
RAAN	53.0738°
Arg of perigee	359.9745°
Mean anomaly	0.1445°
B*	2.0243e-4
Rev at epoch	9,939

▸Two-line element set (TLE)

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

1 61557U 24185F 26188.14072729 .00000480 00000-0 20243-3 0 9997

2 61557 88.9796 53.0738 0009293 359.9745 0.1445 14.24091418 99392

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-24",
  "OBJECT_ID": "2024-185F",
  "EPOCH": "2026-07-07T03:22:38.838+00:00",
  "MEAN_MOTION": 14.24091418,
  "ECCENTRICITY": 0.0009293,
  "INCLINATION": 88.9796,
  "RA_OF_ASC_NODE": 53.0738,
  "ARG_OF_PERICENTER": 359.9745,
  "MEAN_ANOMALY": 0.1445,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61557,
  "REV_AT_EPOCH": 9939,
  "BSTAR": 0.00020243,
  "MEAN_MOTION_DOT": 0.0000048,
  "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-24
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/61557

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