▸Orbital parameters

Orbit class	SSO
Inclination	97.7745°
Eccentricity	0.0000471
Period	96.5 min
Apogee	592 km
Perigee	591 km
Mean motion	14.91995388 rev/day
RAAN	302.1513°
Arg of perigee	130.7662°
Mean anomaly	229.3597°
B*	1.6436e-4
Rev at epoch	5,687

▸Two-line element set (TLE)

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

1 64571U 25135AV 26188.24761321 .00001610 00000-0 16436-3 0 9991

2 64571 97.7745 302.1513 0000471 130.7662 229.3597 14.91995388 56876

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDE-MS2-HEO-5",
  "OBJECT_ID": "2025-135AV",
  "EPOCH": "2026-07-07T05:56:33.781+00:00",
  "MEAN_MOTION": 14.91995388,
  "ECCENTRICITY": 0.0000471,
  "INCLINATION": 97.7745,
  "RA_OF_ASC_NODE": 302.1513,
  "ARG_OF_PERICENTER": 130.7662,
  "MEAN_ANOMALY": 229.3597,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64571,
  "REV_AT_EPOCH": 5687,
  "BSTAR": 0.00016436,
  "MEAN_MOTION_DOT": 0.0000161,
  "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-5
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/64571

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