▸Orbital parameters

Orbit class	SSO
Inclination	97.3980°
Eccentricity	0.0012040
Period	94.8 min
Apogee	516 km
Perigee	499 km
Mean motion	15.19512485 rev/day
RAAN	67.7643°
Arg of perigee	295.0885°
Mean anomaly	64.9100°
B*	2.9867e-4
Rev at epoch	1,519

▸Two-line element set (TLE)

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

1 68409U 26065B 26187.61989756 .00006287 00000-0 29867-3 0 9999

2 68409 97.3980 67.7643 0012040 295.0885 64.9100 15.19512485 15199

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LPNTSAT-002 (IOD-2)",
  "OBJECT_ID": "2026-065B",
  "EPOCH": "2026-07-06T14:52:39.149+00:00",
  "MEAN_MOTION": 15.19512485,
  "ECCENTRICITY": 0.001204,
  "INCLINATION": 97.398,
  "RA_OF_ASC_NODE": 67.7643,
  "ARG_OF_PERICENTER": 295.0885,
  "MEAN_ANOMALY": 64.91,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68409,
  "REV_AT_EPOCH": 1519,
  "BSTAR": 0.00029867,
  "MEAN_MOTION_DOT": 0.00006287,
  "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	LPNTSAT-002 (IOD-2)
Operator	European Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	ItalyMEDIUMvia Wikidata
Launch date	Mar 28, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	30HIGHvia GCAT — Jonathan McDowell's General Catalog 30MEDIUM

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/68409

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