▸Orbital parameters

Orbit class	SSO
Inclination	97.7748°
Eccentricity	0.0001256
Period	96.5 min
Apogee	593 km
Perigee	591 km
Mean motion	14.92006664 rev/day
RAAN	302.0780°
Arg of perigee	133.7507°
Mean anomaly	226.3816°
B*	1.8791e-4
Rev at epoch	5,686

▸Two-line element set (TLE)

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

1 64568U 25135AS 26188.20351436 .00001849 00000-0 18791-3 0 9995

2 64568 97.7748 302.0780 0001256 133.7507 226.3816 14.92006664 56864

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDE-MS2-HEO-3",
  "OBJECT_ID": "2025-135AS",
  "EPOCH": "2026-07-07T04:53:03.641+00:00",
  "MEAN_MOTION": 14.92006664,
  "ECCENTRICITY": 0.0001256,
  "INCLINATION": 97.7748,
  "RA_OF_ASC_NODE": 302.078,
  "ARG_OF_PERICENTER": 133.7507,
  "MEAN_ANOMALY": 226.3816,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64568,
  "REV_AT_EPOCH": 5686,
  "BSTAR": 0.00018791,
  "MEAN_MOTION_DOT": 0.00001849,
  "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	IRIDE-MS2-HEO-3
Operator	Italian Space Agency / ArgoTec srlHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Italy
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	65HIGHvia 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/64568

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