▸Orbital parameters

Orbit class	SSO
Inclination	97.5652°
Eccentricity	0.0017994
Period	95.1 min
Apogee	537 km
Perigee	513 km
Mean motion	15.13718537 rev/day
RAAN	163.2165°
Arg of perigee	190.7024°
Mean anomaly	169.3827°
B*	2.1718e-4
Rev at epoch	7,057

▸Two-line element set (TLE)

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

1 63352U 25061B 26187.89829420 .00003859 00000-0 21718-3 0 9996

2 63352 97.5652 163.2165 0017994 190.7024 169.3827 15.13718537 70578

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-ESPERANZA",
  "OBJECT_ID": "2025-061B",
  "EPOCH": "2026-07-06T21:33:32.619+00:00",
  "MEAN_MOTION": 15.13718537,
  "ECCENTRICITY": 0.0017994,
  "INCLINATION": 97.5652,
  "RA_OF_ASC_NODE": 163.2165,
  "ARG_OF_PERICENTER": 190.7024,
  "MEAN_ANOMALY": 169.3827,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63352,
  "REV_AT_EPOCH": 7057,
  "BSTAR": 0.00021718,
  "MEAN_MOTION_DOT": 0.00003859,
  "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-ESPERANZA
Operator	Orora Technologies GmbHHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Mar 26, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	15HIGHvia 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/63352

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