▸Orbital parameters

Orbit class	SSO
Inclination	97.4077°
Eccentricity	0.0007979
Period	93.4 min
Apogee	447 km
Perigee	436 km
Mean motion	15.41661151 rev/day
RAAN	39.2893°
Arg of perigee	37.3970°
Mean anomaly	322.7831°
B*	3.1040e-4
Rev at epoch	13,540

▸Two-line element set (TLE)

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

1 58903U 24022E 26188.08115866 .00013015 00000-0 31040-3 0 9996

2 58903 97.4077 39.2893 0007979 37.3970 322.7831 15.41661151135406

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-CAEL",
  "OBJECT_ID": "2024-022E",
  "EPOCH": "2026-07-07T01:56:52.108+00:00",
  "MEAN_MOTION": 15.41661151,
  "ECCENTRICITY": 0.0007979,
  "INCLINATION": 97.4077,
  "RA_OF_ASC_NODE": 39.2893,
  "ARG_OF_PERICENTER": 37.397,
  "MEAN_ANOMALY": 322.7831,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58903,
  "REV_AT_EPOCH": 13540,
  "BSTAR": 0.0003104,
  "MEAN_MOTION_DOT": 0.00013015,
  "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-CAEL
Operator	Spire / NorthStar Earth and SpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 31, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	25HIGHvia 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/58903

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