▸Orbital parameters

Orbit class	LEO
Inclination	67.1480°
Eccentricity	0.0007059
Period	103.1 min
Apogee	911 km
Perigee	900 km
Mean motion	13.96673128 rev/day
RAAN	240.8711°
Arg of perigee	274.5477°
Mean anomaly	85.4801°
B*	7.9736e-6
Rev at epoch	13,742

▸Two-line element set (TLE)

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

1 58148U 23165A 26188.16673928 -.00000064 00000-0 79736-5 0 9998

2 58148 67.1480 240.8711 0007059 274.5477 85.4801 13.96673128137423

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2570",
  "OBJECT_ID": "2023-165A",
  "EPOCH": "2026-07-07T04:00:06.274+00:00",
  "MEAN_MOTION": 13.96673128,
  "ECCENTRICITY": 0.0007059,
  "INCLINATION": 67.148,
  "RA_OF_ASC_NODE": 240.8711,
  "ARG_OF_PERICENTER": 274.5477,
  "MEAN_ANOMALY": 85.4801,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58148,
  "REV_AT_EPOCH": 13742,
  "BSTAR": 0.0000079736,
  "MEAN_MOTION_DOT": -6.4e-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	COSMOS 2570
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Oct 27, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	6575HIGHvia 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/58148

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