▸Orbital parameters

Orbit class	SSO
Inclination	97.7751°
Eccentricity	0.0000160
Period	96.5 min
Apogee	592 km
Perigee	592 km
Mean motion	14.92008063 rev/day
RAAN	302.4137°
Arg of perigee	337.4461°
Mean anomaly	22.6751°
B*	1.8757e-4
Rev at epoch	5,688

▸Two-line element set (TLE)

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

1 64587U 25135BM 26188.19243800 .00001846 00000-0 18757-3 0 9998

2 64587 97.7751 302.4137 0000160 337.4461 22.6751 14.92008063 56886

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDE-MS2-HEO-8",
  "OBJECT_ID": "2025-135BM",
  "EPOCH": "2026-07-07T04:37:06.643+00:00",
  "MEAN_MOTION": 14.92008063,
  "ECCENTRICITY": 0.000016,
  "INCLINATION": 97.7751,
  "RA_OF_ASC_NODE": 302.4137,
  "ARG_OF_PERICENTER": 337.4461,
  "MEAN_ANOMALY": 22.6751,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64587,
  "REV_AT_EPOCH": 5688,
  "BSTAR": 0.00018757,
  "MEAN_MOTION_DOT": 0.00001846,
  "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-8
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/64587

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