▸Orbital parameters

Orbit class	LEO
Inclination	88.9780°
Eccentricity	0.0007854
Period	102.7 min
Apogee	891 km
Perigee	880 km
Mean motion	14.02481455 rev/day
RAAN	55.0959°
Arg of perigee	50.6487°
Mean anomaly	309.5388°
B*	1.7338e-4
Rev at epoch	9,827

▸Two-line element set (TLE)

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

1 61567U 24185R 26188.07325888 .00000280 00000-0 17338-3 0 9996

2 61567 88.9780 55.0959 0007854 50.6487 309.5388 14.02481455 98270

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-34",
  "OBJECT_ID": "2024-185R",
  "EPOCH": "2026-07-07T01:45:29.567+00:00",
  "MEAN_MOTION": 14.02481455,
  "ECCENTRICITY": 0.0007854,
  "INCLINATION": 88.978,
  "RA_OF_ASC_NODE": 55.0959,
  "ARG_OF_PERICENTER": 50.6487,
  "MEAN_ANOMALY": 309.5388,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61567,
  "REV_AT_EPOCH": 9827,
  "BSTAR": 0.00017338,
  "MEAN_MOTION_DOT": 0.0000028,
  "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-34
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/61567

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