▸Orbital parameters

Orbit class	SSO
Inclination	97.6883°
Eccentricity	0.0002286
Period	96.1 min
Apogee	576 km
Perigee	572 km
Mean motion	14.97742162 rev/day
RAAN	80.1499°
Arg of perigee	65.5794°
Mean anomaly	294.5666°
B*	2.8529e-4
Rev at epoch	7,161

▸Two-line element set (TLE)

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

1 63259U 25052BB 26187.69387654 .00003288 00000-0 28529-3 0 9991

2 63259 97.6883 80.1499 0002286 65.5794 294.5666 14.97742162 71619

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-DELOITTE-1",
  "OBJECT_ID": "2025-052BB",
  "EPOCH": "2026-07-06T16:39:10.933+00:00",
  "MEAN_MOTION": 14.97742162,
  "ECCENTRICITY": 0.0002286,
  "INCLINATION": 97.6883,
  "RA_OF_ASC_NODE": 80.1499,
  "ARG_OF_PERICENTER": 65.5794,
  "MEAN_ANOMALY": 294.5666,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63259,
  "REV_AT_EPOCH": 7161,
  "BSTAR": 0.00028529,
  "MEAN_MOTION_DOT": 0.00003288,
  "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-DELOITTE-1
Operator	Deloitte Space, El Segundo / SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/63259

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