▸Orbital parameters

Orbit class	SSO
Inclination	97.2864°
Eccentricity	0.0003420
Period	93.4 min
Apogee	445 km
Perigee	441 km
Mean motion	15.41116239 rev/day
RAAN	254.3973°
Arg of perigee	266.1752°
Mean anomaly	93.9104°
B*	2.1600e-4
Rev at epoch	24,891

▸Two-line element set (TLE)

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

1 51060U 22002CE 26188.14522347 .00008858 00000-0 21600-3 0 9992

2 51060 97.2864 254.3973 0003420 266.1752 93.9104 15.41116239248914

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ETV-A1",
  "OBJECT_ID": "2022-002CE",
  "EPOCH": "2026-07-07T03:29:07.308+00:00",
  "MEAN_MOTION": 15.41116239,
  "ECCENTRICITY": 0.000342,
  "INCLINATION": 97.2864,
  "RA_OF_ASC_NODE": 254.3973,
  "ARG_OF_PERICENTER": 266.1752,
  "MEAN_ANOMALY": 93.9104,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 51060,
  "REV_AT_EPOCH": 24891,
  "BSTAR": 0.000216,
  "MEAN_MOTION_DOT": 0.00008858,
  "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	ETV-A1
Operator	Sen Corporation LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Jan 13, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/51060

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