▸Orbital parameters

Orbit class	LEO
Inclination	45.3926°
Eccentricity	0.0008364
Period	94.2 min
Apogee	488 km
Perigee	476 km
Mean motion	15.27976863 rev/day
RAAN	13.9564°
Arg of perigee	202.7682°
Mean anomaly	157.2838°
B*	8.2702e-4
Rev at epoch	3,744

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 66295U 25248C 26186.82496654 .00022785 00000-0 82702-3 0 9992

2 66295 45.3926 13.9564 0008364 202.7682 157.2838 15.27976863 37441

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-AFFIE-WAUWIE",
  "OBJECT_ID": "2025-248C",
  "EPOCH": "2026-07-05T19:47:57.109+00:00",
  "MEAN_MOTION": 15.27976863,
  "ECCENTRICITY": 0.0008364,
  "INCLINATION": 45.3926,
  "RA_OF_ASC_NODE": 13.9564,
  "ARG_OF_PERICENTER": 202.7682,
  "MEAN_ANOMALY": 157.2838,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66295,
  "REV_AT_EPOCH": 3744,
  "BSTAR": 0.00082702,
  "MEAN_MOTION_DOT": 0.00022785,
  "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-AFFIE-WAUWIE
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Nov 2, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	7.6HIGHvia 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/66295

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