▸Orbital parameters

Orbit class	SSO
Inclination	97.5243°
Eccentricity	0.0004393
Period	96.0 min
Apogee	568 km
Perigee	562 km
Mean motion	15.00493817 rev/day
RAAN	258.0885°
Arg of perigee	79.4597°
Mean anomaly	280.7122°
B*	3.2922e-4
Rev at epoch	3,308

▸Two-line element set (TLE)

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

1 66785U 25276EA 26187.76888705 .00004091 00000-0 32922-3 0 9992

2 66785 97.5243 258.0885 0004393 79.4597 280.7122 15.00493817 33084

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-VUKASIN",
  "OBJECT_ID": "2025-276EA",
  "EPOCH": "2026-07-06T18:27:11.841+00:00",
  "MEAN_MOTION": 15.00493817,
  "ECCENTRICITY": 0.0004393,
  "INCLINATION": 97.5243,
  "RA_OF_ASC_NODE": 258.0885,
  "ARG_OF_PERICENTER": 79.4597,
  "MEAN_ANOMALY": 280.7122,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66785,
  "REV_AT_EPOCH": 3308,
  "BSTAR": 0.00032922,
  "MEAN_MOTION_DOT": 0.00004091,
  "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	LEMUR-2-VUKASIN
Operator	Spire / Lacuna SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Nov 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5HIGHvia 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/66785

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