▸Orbital parameters

Orbit class	LEO
Inclination	88.9825°
Eccentricity	0.0006565
Period	100.8 min
Apogee	802 km
Perigee	792 km
Mean motion	14.28411764 rev/day
RAAN	52.7642°
Arg of perigee	349.8737°
Mean anomaly	10.2325°
B*	2.1205e-4
Rev at epoch	9,963

▸Two-line element set (TLE)

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

1 61561U 24185K 26188.13020118 .00000545 00000-0 21205-3 0 9997

2 61561 88.9825 52.7642 0006565 349.8737 10.2325 14.28411764 99638

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-28",
  "OBJECT_ID": "2024-185K",
  "EPOCH": "2026-07-07T03:07:29.382+00:00",
  "MEAN_MOTION": 14.28411764,
  "ECCENTRICITY": 0.0006565,
  "INCLINATION": 88.9825,
  "RA_OF_ASC_NODE": 52.7642,
  "ARG_OF_PERICENTER": 349.8737,
  "MEAN_ANOMALY": 10.2325,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61561,
  "REV_AT_EPOCH": 9963,
  "BSTAR": 0.00021205,
  "MEAN_MOTION_DOT": 0.00000545,
  "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-28
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/61561

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