▸Orbital parameters

Orbit class	SSO
Inclination	97.4139°
Eccentricity	0.0002346
Period	94.7 min
Apogee	504 km
Perigee	500 km
Mean motion	15.21279534 rev/day
RAAN	261.6395°
Arg of perigee	96.4598°
Mean anomaly	263.6905°
B*	1.7344e-4
Rev at epoch	3,348

▸Two-line element set (TLE)

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

1 66768U 25276DG 26188.17884817 .00003808 00000-0 17344-3 0 9995

2 66768 97.4139 261.6395 0002346 96.4598 263.6905 15.21279534 33484

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-TEODOR",
  "OBJECT_ID": "2025-276DG",
  "EPOCH": "2026-07-07T04:17:32.482+00:00",
  "MEAN_MOTION": 15.21279534,
  "ECCENTRICITY": 0.0002346,
  "INCLINATION": 97.4139,
  "RA_OF_ASC_NODE": 261.6395,
  "ARG_OF_PERICENTER": 96.4598,
  "MEAN_ANOMALY": 263.6905,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66768,
  "REV_AT_EPOCH": 3348,
  "BSTAR": 0.00017344,
  "MEAN_MOTION_DOT": 0.00003808,
  "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-TEODOR
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/66768

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