▸Orbital parameters

Orbit class	SSO
Inclination	97.7564°
Eccentricity	0.0003805
Period	96.5 min
Apogee	595 km
Perigee	589 km
Mean motion	14.91908202 rev/day
RAAN	145.7182°
Arg of perigee	21.9974°
Mean anomaly	338.1407°
B*	3.4970e-4
Rev at epoch	1,465

▸Two-line element set (TLE)

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

1 68492U 26067CE 26187.85892434 .00003481 00000-0 34970-3 0 9999

2 68492 97.7564 145.7182 0003805 21.9974 338.1407 14.91908202 14653

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-EMARCHIA",
  "OBJECT_ID": "2026-067CE",
  "EPOCH": "2026-07-06T20:36:51.063+00:00",
  "MEAN_MOTION": 14.91908202,
  "ECCENTRICITY": 0.0003805,
  "INCLINATION": 97.7564,
  "RA_OF_ASC_NODE": 145.7182,
  "ARG_OF_PERICENTER": 21.9974,
  "MEAN_ANOMALY": 338.1407,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68492,
  "REV_AT_EPOCH": 1465,
  "BSTAR": 0.0003497,
  "MEAN_MOTION_DOT": 0.00003481,
  "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-EMARCHIA
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/68492

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