▸Orbital parameters

Orbit class	SSO
Inclination	97.7341°
Eccentricity	0.0006647
Period	96.6 min
Apogee	599 km
Perigee	590 km
Mean motion	14.91062989 rev/day
RAAN	85.1736°
Arg of perigee	83.2956°
Mean anomaly	276.9019°
B*	1.2781e-4
Rev at epoch	967

▸Two-line element set (TLE)

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

1 68981U 26100B 26188.15986250 .00001211 00000-0 12781-3 0 9999

2 68981 97.7341 85.1736 0006647 83.2956 276.9019 14.91062989 9676

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDE-MS2-HEO-7",
  "OBJECT_ID": "2026-100B",
  "EPOCH": "2026-07-07T03:50:12.12+00:00",
  "MEAN_MOTION": 14.91062989,
  "ECCENTRICITY": 0.0006647,
  "INCLINATION": 97.7341,
  "RA_OF_ASC_NODE": 85.1736,
  "ARG_OF_PERICENTER": 83.2956,
  "MEAN_ANOMALY": 276.9019,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68981,
  "REV_AT_EPOCH": 967,
  "BSTAR": 0.00012781,
  "MEAN_MOTION_DOT": 0.00001211,
  "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-7
Operator	Italian Space Agency / ArgoTec srlHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Italy
Launch date	May 3, 2026HIGHvia 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/68981

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