▸Orbital parameters

Orbit class	SSO
Inclination	97.4512°
Eccentricity	0.0002251
Period	94.0 min
Apogee	473 km
Perigee	470 km
Mean motion	15.31349669 rev/day
RAAN	304.5274°
Arg of perigee	260.9764°
Mean anomaly	99.1222°
B*	1.9213e-4
Rev at epoch	14,039

▸Two-line element set (TLE)

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

1 58663U 23208D 26188.20072801 .00005738 00000-0 19213-3 0 9990

2 58663 97.4512 304.5274 0002251 260.9764 99.1222 15.31349669140396

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TIANMU-1 22",
  "OBJECT_ID": "2023-208D",
  "EPOCH": "2026-07-07T04:49:02.9+00:00",
  "MEAN_MOTION": 15.31349669,
  "ECCENTRICITY": 0.0002251,
  "INCLINATION": 97.4512,
  "RA_OF_ASC_NODE": 304.5274,
  "ARG_OF_PERICENTER": 260.9764,
  "MEAN_ANOMALY": 99.1222,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58663,
  "REV_AT_EPOCH": 14039,
  "BSTAR": 0.00019213,
  "MEAN_MOTION_DOT": 0.00005738,
  "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	TIANMU-1 22
Operator	Aerospace Tianmu Satellite Tech. Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 27, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia 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/58663

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