▸Orbital parameters

Orbit class	SSO
Inclination	97.6845°
Eccentricity	0.0000931
Period	96.2 min
Apogee	575 km
Perigee	574 km
Mean motion	14.97533628 rev/day
RAAN	80.1714°
Arg of perigee	26.9375°
Mean anomaly	333.1895°
B*	2.8661e-4
Rev at epoch	7,167

▸Two-line element set (TLE)

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

1 63264U 25052BG 26188.12404301 .00003286 00000-0 28661-3 0 9990

2 63264 97.6845 80.1714 0000931 26.9375 333.1895 14.97533628 71679

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-THEFALCONER",
  "OBJECT_ID": "2025-052BG",
  "EPOCH": "2026-07-07T02:58:37.316+00:00",
  "MEAN_MOTION": 14.97533628,
  "ECCENTRICITY": 0.0000931,
  "INCLINATION": 97.6845,
  "RA_OF_ASC_NODE": 80.1714,
  "ARG_OF_PERICENTER": 26.9375,
  "MEAN_ANOMALY": 333.1895,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63264,
  "REV_AT_EPOCH": 7167,
  "BSTAR": 0.00028661,
  "MEAN_MOTION_DOT": 0.00003286,
  "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-THEFALCONER
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/63264

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