▸Orbital parameters

Orbit class	SSO
Inclination	97.5032°
Eccentricity	0.0001677
Period	96.2 min
Apogee	580 km
Perigee	577 km
Mean motion	14.96260095 rev/day
RAAN	59.6809°
Arg of perigee	75.5315°
Mean anomaly	284.6093°
B*	6.6751e-5
Rev at epoch	42,592

▸Two-line element set (TLE)

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

1 43619U 18071B 26188.18380176 .00000699 00000-0 66751-4 0 9992

2 43619 97.5032 59.6809 0001677 75.5315 284.6093 14.96260095425921

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NOVASAR 1",
  "OBJECT_ID": "2018-071B",
  "EPOCH": "2026-07-07T04:24:40.472+00:00",
  "MEAN_MOTION": 14.96260095,
  "ECCENTRICITY": 0.0001677,
  "INCLINATION": 97.5032,
  "RA_OF_ASC_NODE": 59.6809,
  "ARG_OF_PERICENTER": 75.5315,
  "MEAN_ANOMALY": 284.6093,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43619,
  "REV_AT_EPOCH": 42592,
  "BSTAR": 0.000066751,
  "MEAN_MOTION_DOT": 0.00000699,
  "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	NOVASAR 1
Operator	Surrey Satellite Technology Ltd/AstriumHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Sep 16, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	445HIGHvia 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/43619

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