▸Orbital parameters

Orbit class	SSO
Inclination	97.2909°
Eccentricity	0.0004563
Period	92.6 min
Apogee	404 km
Perigee	398 km
Mean motion	15.55353845 rev/day
RAAN	64.5318°
Arg of perigee	176.4235°
Mean anomaly	183.7053°
B*	3.7132e-4
Rev at epoch	13,752

▸Two-line element set (TLE)

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

1 61769U 24199AL 26188.15562730 .00025169 00000-0 37132-3 0 9990

2 61769 97.2909 64.5318 0004563 176.4235 183.7053 15.55353845137529

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KOSAR",
  "OBJECT_ID": "2024-199AL",
  "EPOCH": "2026-07-07T03:44:06.199+00:00",
  "MEAN_MOTION": 15.55353845,
  "ECCENTRICITY": 0.0004563,
  "INCLINATION": 97.2909,
  "RA_OF_ASC_NODE": 64.5318,
  "ARG_OF_PERICENTER": 176.4235,
  "MEAN_ANOMALY": 183.7053,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61769,
  "REV_AT_EPOCH": 13752,
  "BSTAR": 0.00037132,
  "MEAN_MOTION_DOT": 0.00025169,
  "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	KOSAR
Operator	SpaceOMID Co. LLC / Iran Space Research InstituteHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Iran
Launch date	Nov 4, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	30HIGHvia 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/61769

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