▸Orbital parameters

Orbit class	SSO
Inclination	97.7634°
Eccentricity	0.0003330
Period	96.4 min
Apogee	591 km
Perigee	586 km
Mean motion	14.93058344 rev/day
RAAN	145.5102°
Arg of perigee	176.2361°
Mean anomaly	183.8884°
B*	4.0763e-4
Rev at epoch	1,459

▸Two-line element set (TLE)

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

1 68480U 26067BS 26187.36758502 .00004188 00000-0 40763-3 0 9991

2 68480 97.7634 145.5102 0003330 176.2361 183.8884 14.93058344 14597

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-IRINA",
  "OBJECT_ID": "2026-067BS",
  "EPOCH": "2026-07-06T08:49:19.346+00:00",
  "MEAN_MOTION": 14.93058344,
  "ECCENTRICITY": 0.00033297,
  "INCLINATION": 97.7634,
  "RA_OF_ASC_NODE": 145.5102,
  "ARG_OF_PERICENTER": 176.2361,
  "MEAN_ANOMALY": 183.8884,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68480,
  "REV_AT_EPOCH": 1459,
  "BSTAR": 0.00040762836,
  "MEAN_MOTION_DOT": 0.00004188,
  "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-IRINA
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 30, 2026HIGHvia 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/68480

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