▸Orbital parameters

Orbit class	SSO
Inclination	97.6861°
Eccentricity	0.0005203
Period	96.1 min
Apogee	577 km
Perigee	570 km
Mean motion	14.97976249 rev/day
RAAN	79.7730°
Arg of perigee	111.5295°
Mean anomaly	248.6482°
B*	3.9684e-4
Rev at epoch	7,159

▸Two-line element set (TLE)

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

1 63248U 25052AQ 26187.64800424 .00004626 00000-0 39684-3 0 9990

2 63248 97.6861 79.7730 0005203 111.5295 248.6482 14.97976249 71593

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-LIA-MARTIN",
  "OBJECT_ID": "2025-052AQ",
  "EPOCH": "2026-07-06T15:33:07.566+00:00",
  "MEAN_MOTION": 14.97976249,
  "ECCENTRICITY": 0.0005203,
  "INCLINATION": 97.6861,
  "RA_OF_ASC_NODE": 79.773,
  "ARG_OF_PERICENTER": 111.5295,
  "MEAN_ANOMALY": 248.6482,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63248,
  "REV_AT_EPOCH": 7159,
  "BSTAR": 0.00039684,
  "MEAN_MOTION_DOT": 0.00004626,
  "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-LIA-MARTIN
Operator	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/63248

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