▸Orbital parameters

Orbit class	SSO
Inclination	97.5690°
Eccentricity	0.0009019
Period	95.1 min
Apogee	532 km
Perigee	519 km
Mean motion	15.13547175 rev/day
RAAN	279.7688°
Arg of perigee	176.6122°
Mean anomaly	183.5172°
B*	2.6837e-4
Rev at epoch	11,494

▸Two-line element set (TLE)

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

1 60012U 24110A 26188.22467741 .00004749 00000-0 26837-3 0 9998

2 60012 97.5690 279.7688 0009019 176.6122 183.5172 15.13547175114943

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-110A",
  "OBJECT_ID": "2024-110A",
  "EPOCH": "2026-07-07T05:23:32.128+00:00",
  "MEAN_MOTION": 15.13547175,
  "ECCENTRICITY": 0.0009019,
  "INCLINATION": 97.569,
  "RA_OF_ASC_NODE": 279.7688,
  "ARG_OF_PERICENTER": 176.6122,
  "MEAN_ANOMALY": 183.5172,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60012,
  "REV_AT_EPOCH": 11494,
  "BSTAR": 0.00026837,
  "MEAN_MOTION_DOT": 0.00004749,
  "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	2024-110A
Operator	Mumei Star TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 6, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	112HIGHvia 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/60012

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