▸Orbital parameters

Orbit class	SSO
Inclination	97.6871°
Eccentricity	0.0002783
Period	95.3 min
Apogee	533 km
Perigee	529 km
Mean motion	15.11670752 rev/day
RAAN	271.2045°
Arg of perigee	81.1160°
Mean anomaly	279.0384°
B*	4.7483e-4
Rev at epoch	10,350

▸Two-line element set (TLE)

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

1 60536U 24149BW 26188.18785465 .00008016 00000-0 47483-3 0 9993

2 60536 97.6871 271.2045 0002783 81.1160 279.0384 15.11670752103505

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-MARHISYAM",
  "OBJECT_ID": "2024-149BW",
  "EPOCH": "2026-07-07T04:30:30.642+00:00",
  "MEAN_MOTION": 15.11670752,
  "ECCENTRICITY": 0.0002783,
  "INCLINATION": 97.6871,
  "RA_OF_ASC_NODE": 271.2045,
  "ARG_OF_PERICENTER": 81.116,
  "MEAN_ANOMALY": 279.0384,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60536,
  "REV_AT_EPOCH": 10350,
  "BSTAR": 0.00047483,
  "MEAN_MOTION_DOT": 0.00008016,
  "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-MARHISYAM
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia 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/60536

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