▸Orbital parameters

Orbit class	SSO
Inclination	97.6846°
Eccentricity	0.0003575
Period	96.3 min
Apogee	586 km
Perigee	581 km
Mean motion	14.94638806 rev/day
RAAN	78.9545°
Arg of perigee	128.0783°
Mean anomaly	232.0761°
B*	1.6883e-4
Rev at epoch	7,159

▸Two-line element set (TLE)

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

1 63252U 25052AU 26188.16692324 .00001773 00000-0 16883-3 0 9997

2 63252 97.6846 78.9545 0003575 128.0783 232.0761 14.94638806 71599

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ARVAKER-1",
  "OBJECT_ID": "2025-052AU",
  "EPOCH": "2026-07-07T04:00:22.168+00:00",
  "MEAN_MOTION": 14.94638806,
  "ECCENTRICITY": 0.0003575,
  "INCLINATION": 97.6846,
  "RA_OF_ASC_NODE": 78.9545,
  "ARG_OF_PERICENTER": 128.0783,
  "MEAN_ANOMALY": 232.0761,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63252,
  "REV_AT_EPOCH": 7159,
  "BSTAR": 0.00016883,
  "MEAN_MOTION_DOT": 0.00001773,
  "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-1
Operator	Norwegian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Norway
Launch date	Mar 15, 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/63252

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