▸Orbital parameters

Orbit class	SSO
Inclination	97.3685°
Eccentricity	0.0007107
Period	93.8 min
Apogee	464 km
Perigee	454 km
Mean motion	15.35678970 rev/day
RAAN	8.5318°
Arg of perigee	293.7973°
Mean anomaly	66.2525°
B*	5.1664e-4
Rev at epoch	49,145

▸Two-line element set (TLE)

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

1 42838U 17042P 26187.73544480 .00017878 00000-0 51664-3 0 9994

2 42838 97.3685 8.5318 0007107 293.7973 66.2525 15.35678970491455

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-ANDIS",
  "OBJECT_ID": "2017-042P",
  "EPOCH": "2026-07-06T17:39:02.431+00:00",
  "MEAN_MOTION": 15.3567897,
  "ECCENTRICITY": 0.0007107,
  "INCLINATION": 97.3685,
  "RA_OF_ASC_NODE": 8.5318,
  "ARG_OF_PERICENTER": 293.7973,
  "MEAN_ANOMALY": 66.2525,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 42838,
  "REV_AT_EPOCH": 49145,
  "BSTAR": 0.00051664,
  "MEAN_MOTION_DOT": 0.00017878,
  "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-ANDIS
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jul 14, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia 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/42838

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