▸Orbital parameters

Orbit class	SSO
Inclination	97.7753°
Eccentricity	0.0000851
Period	96.4 min
Apogee	587 km
Perigee	586 km
Mean motion	14.93638329 rev/day
RAAN	302.1359°
Arg of perigee	162.1976°
Mean anomaly	197.9274°
B*	2.2141e-4
Rev at epoch	5,686

▸Two-line element set (TLE)

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

1 64567U 25135AR 26188.19865215 .00002282 00000-0 22141-3 0 9993

2 64567 97.7753 302.1359 0000851 162.1976 197.9274 14.93638329 56869

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ARVAKER-2",
  "OBJECT_ID": "2025-135AR",
  "EPOCH": "2026-07-07T04:46:03.546+00:00",
  "MEAN_MOTION": 14.93638329,
  "ECCENTRICITY": 0.0000851,
  "INCLINATION": 97.7753,
  "RA_OF_ASC_NODE": 302.1359,
  "ARG_OF_PERICENTER": 162.1976,
  "MEAN_ANOMALY": 197.9274,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64567,
  "REV_AT_EPOCH": 5686,
  "BSTAR": 0.00022141,
  "MEAN_MOTION_DOT": 0.00002282,
  "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	ARVAKER-2
Operator	Norwegian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Norway
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	100HIGHvia 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/64567

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