▸Orbital parameters

Orbit class	SSO
Inclination	97.6951°
Eccentricity	0.0003408
Period	95.8 min
Apogee	560 km
Perigee	555 km
Mean motion	15.03089428 rev/day
RAAN	270.0782°
Arg of perigee	155.6076°
Mean anomaly	204.5311°
B*	4.8274e-4
Rev at epoch	10,314

▸Two-line element set (TLE)

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

1 62706U 25009DB 26188.04282409 .00006452 00000-0 48274-3 0 9996

2 62706 97.6951 270.0782 0003408 155.6076 204.5311 15.03089428103146

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-ALISIA",
  "OBJECT_ID": "2025-009DB",
  "EPOCH": "2026-07-07T01:01:40.001+00:00",
  "MEAN_MOTION": 15.03089428,
  "ECCENTRICITY": 0.0003408,
  "INCLINATION": 97.6951,
  "RA_OF_ASC_NODE": 270.0782,
  "ARG_OF_PERICENTER": 155.6076,
  "MEAN_ANOMALY": 204.5311,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62706,
  "REV_AT_EPOCH": 10314,
  "BSTAR": 0.00048274,
  "MEAN_MOTION_DOT": 0.00006452,
  "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-ALISIA
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 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/62706

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