▸Orbital parameters

Orbit class	SSO
Inclination	98.7147°
Eccentricity	0.0000320
Period	101.2 min
Apogee	816 km
Perigee	816 km
Mean motion	14.22761338 rev/day
RAAN	61.0000°
Arg of perigee	79.2971°
Mean anomaly	280.8243°
B*	3.2992e-5
Rev at epoch	13,366

▸Two-line element set (TLE)

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

1 61736U 24199B 26188.13025208 .00000030 00000-0 32992-4 0 9996

2 61736 98.7147 61.0000 0000320 79.2971 280.8243 14.22761338133661

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IONOSFERA-M 2",
  "OBJECT_ID": "2024-199B",
  "EPOCH": "2026-07-07T03:07:33.78+00:00",
  "MEAN_MOTION": 14.22761338,
  "ECCENTRICITY": 0.000032,
  "INCLINATION": 98.7147,
  "RA_OF_ASC_NODE": 61,
  "ARG_OF_PERICENTER": 79.2971,
  "MEAN_ANOMALY": 280.8243,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61736,
  "REV_AT_EPOCH": 13366,
  "BSTAR": 0.000032992,
  "MEAN_MOTION_DOT": 3e-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	IONOSFERA-M 2
Operator	Joint Stock Corp. VNIIEMHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Nov 4, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	430HIGHvia 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/61736

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