▸Orbital parameters

Orbit class	SSO
Inclination	97.3945°
Eccentricity	0.0006354
Period	94.2 min
Apogee	483 km
Perigee	474 km
Mean motion	15.29036711 rev/day
RAAN	82.4569°
Arg of perigee	83.0826°
Mean anomaly	277.1137°
B*	2.2938e-4
Rev at epoch	7,300

▸Two-line element set (TLE)

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

1 63834U 25052BQ 26188.15069586 .00006395 00000-0 22938-3 0 9993

2 63834 97.3945 82.4569 0006354 83.0826 277.1137 15.29036711 73005

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HERMES-5",
  "OBJECT_ID": "2025-052BQ",
  "EPOCH": "2026-07-07T03:37:00.122+00:00",
  "MEAN_MOTION": 15.29036711,
  "ECCENTRICITY": 0.0006354,
  "INCLINATION": 97.3945,
  "RA_OF_ASC_NODE": 82.4569,
  "ARG_OF_PERICENTER": 83.0826,
  "MEAN_ANOMALY": 277.1137,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63834,
  "REV_AT_EPOCH": 7300,
  "BSTAR": 0.00022938,
  "MEAN_MOTION_DOT": 0.00006395,
  "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	HERMES-5
Operator	Italian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Italy
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5HIGHvia 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/63834

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