▸Orbital parameters

Orbit class	SSO
Inclination	97.4199°
Eccentricity	0.0004165
Period	94.7 min
Apogee	509 km
Perigee	503 km
Mean motion	15.19992779 rev/day
RAAN	261.2790°
Arg of perigee	292.5892°
Mean anomaly	67.4902°
B*	2.3128e-4
Rev at epoch	3,344

▸Two-line element set (TLE)

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

1 66678U 25276N 26188.13186521 .00004913 00000-0 23128-3 0 9993

2 66678 97.4199 261.2790 0004165 292.5892 67.4902 15.19992779 33445

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-DEANANDMAEVE",
  "OBJECT_ID": "2025-276N",
  "EPOCH": "2026-07-07T03:09:53.154+00:00",
  "MEAN_MOTION": 15.19992779,
  "ECCENTRICITY": 0.0004165,
  "INCLINATION": 97.4199,
  "RA_OF_ASC_NODE": 261.279,
  "ARG_OF_PERICENTER": 292.5892,
  "MEAN_ANOMALY": 67.4902,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66678,
  "REV_AT_EPOCH": 3344,
  "BSTAR": 0.00023128,
  "MEAN_MOTION_DOT": 0.00004913,
  "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-DEANANDMAEVE
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Nov 28, 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/66678

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