▸Orbital parameters

Orbit class	SSO
Inclination	97.4689°
Eccentricity	0.0001131
Period	94.6 min
Apogee	499 km
Perigee	498 km
Mean motion	15.22503644 rev/day
RAAN	303.3695°
Arg of perigee	134.9080°
Mean anomaly	225.2249°
B*	1.3919e-4
Rev at epoch	5,792

▸Two-line element set (TLE)

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

1 64552U 25135AA 26188.17529359 .00003154 00000-0 13919-3 0 9993

2 64552 97.4689 303.3695 0001131 134.9080 225.2249 15.22503644 57928

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HYPERFIELD-1B",
  "OBJECT_ID": "2025-135AA",
  "EPOCH": "2026-07-07T04:12:25.366+00:00",
  "MEAN_MOTION": 15.22503644,
  "ECCENTRICITY": 0.0001131,
  "INCLINATION": 97.4689,
  "RA_OF_ASC_NODE": 303.3695,
  "ARG_OF_PERICENTER": 134.908,
  "MEAN_ANOMALY": 225.2249,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64552,
  "REV_AT_EPOCH": 5792,
  "BSTAR": 0.00013919,
  "MEAN_MOTION_DOT": 0.00003154,
  "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	HYPERFIELD-1B
Operator	Kuva Space OyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Finland
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia 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/64552

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