▸Orbital parameters

Orbit class	SSO
Inclination	97.7042°
Eccentricity	0.0001586
Period	96.3 min
Apogee	583 km
Perigee	581 km
Mean motion	14.95120255 rev/day
RAAN	266.0863°
Arg of perigee	29.9903°
Mean anomaly	330.1408°
B*	1.1556e-4
Rev at epoch	8,028

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62702U 25009CX 26187.72157389 .00001211 00000-0 11556-3 0 9995

2 62702 97.7042 266.0863 0001586 29.9903 330.1408 14.95120255 80282

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NORSAT 4",
  "OBJECT_ID": "2025-009CX",
  "EPOCH": "2026-07-06T17:19:03.984+00:00",
  "MEAN_MOTION": 14.95120255,
  "ECCENTRICITY": 0.0001586,
  "INCLINATION": 97.7042,
  "RA_OF_ASC_NODE": 266.0863,
  "ARG_OF_PERICENTER": 29.9903,
  "MEAN_ANOMALY": 330.1408,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62702,
  "REV_AT_EPOCH": 8028,
  "BSTAR": 0.00011556,
  "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	NORSAT 4
Operator	Norwegian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Norway
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	35HIGHvia 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/62702

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