▸Orbital parameters

Orbit class	SSO
Inclination	97.7713°
Eccentricity	0.0001958
Period	96.4 min
Apogee	588 km
Perigee	585 km
Mean motion	14.93668565 rev/day
RAAN	301.8414°
Arg of perigee	185.7191°
Mean anomaly	174.4007°
B*	1.0832e-4
Rev at epoch	5,685

▸Two-line element set (TLE)

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

1 64565U 25135AP 26188.16933992 .00001088 00000-0 10832-3 0 9993

2 64565 97.7713 301.8414 0001958 185.7191 174.4007 14.93668565 56858

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-HUBBLE-4",
  "OBJECT_ID": "2025-135AP",
  "EPOCH": "2026-07-07T04:03:50.969+00:00",
  "MEAN_MOTION": 14.93668565,
  "ECCENTRICITY": 0.0001958,
  "INCLINATION": 97.7713,
  "RA_OF_ASC_NODE": 301.8414,
  "ARG_OF_PERICENTER": 185.7191,
  "MEAN_ANOMALY": 174.4007,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64565,
  "REV_AT_EPOCH": 5685,
  "BSTAR": 0.00010832,
  "MEAN_MOTION_DOT": 0.00001088,
  "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-HUBBLE-4
Operator	Hubble Network Inc. / Spire/GlasgowHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	22HIGHvia 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/64565

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