▸Orbital parameters

Orbit class	LEO
Inclination	89.0094°
Eccentricity	0.0020606
Period	104.8 min
Apogee	1,001 km
Perigee	971 km
Mean motion	13.73880406 rev/day
RAAN	20.0796°
Arg of perigee	50.8287°
Mean anomaly	309.4704°
B*	2.4927e-5
Rev at epoch	710

▸Two-line element set (TLE)

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

1 69112U 26108J 26188.12892800 .00000036 00000-0 24927-4 0 9998

2 69112 89.0094 20.0796 0020606 50.8287 309.4704 13.73880406 7104

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-153",
  "OBJECT_ID": "2026-108J",
  "EPOCH": "2026-07-07T03:05:39.379+00:00",
  "MEAN_MOTION": 13.73880406,
  "ECCENTRICITY": 0.0020606,
  "INCLINATION": 89.0094,
  "RA_OF_ASC_NODE": 20.0796,
  "ARG_OF_PERICENTER": 50.8287,
  "MEAN_ANOMALY": 309.4704,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69112,
  "REV_AT_EPOCH": 710,
  "BSTAR": 0.000024927,
  "MEAN_MOTION_DOT": 3.6e-7,
  "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-153
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 17, 2026HIGHvia 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/69112

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