▸Orbital parameters

Orbit class	HEO
Inclination	62.6814°
Eccentricity	0.6789282
Period	717.8 min
Apogee	38,208 km
Perigee	2,148 km
Mean motion	2.00610858 rev/day
RAAN	138.6582°
Arg of perigee	272.8476°
Mean anomaly	17.6287°
B*	0.0000e+0
Rev at epoch	3,142

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 52145U 22030A 26187.90870368 .00000208 00000-0 00000-0 0 9999

2 52145 62.6814 138.6582 6789282 272.8476 17.6287 2.00610858 31428

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MERIDIAN 10",
  "OBJECT_ID": "2022-030A",
  "EPOCH": "2026-07-06T21:48:31.998+00:00",
  "MEAN_MOTION": 2.00610858,
  "ECCENTRICITY": 0.6789282,
  "INCLINATION": 62.6814,
  "RA_OF_ASC_NODE": 138.6582,
  "ARG_OF_PERICENTER": 272.8476,
  "MEAN_ANOMALY": 17.6287,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52145,
  "REV_AT_EPOCH": 3142,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000208,
  "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	MERIDIAN 10
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Mar 22, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2000HIGHvia 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/52145

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