▸Orbital parameters

Orbit class	SSO
Inclination	97.5452°
Eccentricity	0.0005435
Period	92.7 min
Apogee	410 km
Perigee	403 km
Mean motion	15.53491971 rev/day
RAAN	337.9495°
Arg of perigee	131.7519°
Mean anomaly	228.4199°
B*	6.3669e-4
Rev at epoch	13,091

▸Two-line element set (TLE)

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

1 59148U 24043BC 26188.19073939 .00040476 00000-0 63669-3 0 9990

2 59148 97.5452 337.9495 0005435 131.7519 228.4199 15.53491971130919

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HAMMER",
  "OBJECT_ID": "2024-043BC",
  "EPOCH": "2026-07-07T04:34:39.883+00:00",
  "MEAN_MOTION": 15.53491971,
  "ECCENTRICITY": 0.0005435,
  "INCLINATION": 97.5452,
  "RA_OF_ASC_NODE": 337.9495,
  "ARG_OF_PERICENTER": 131.7519,
  "MEAN_ANOMALY": 228.4199,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59148,
  "REV_AT_EPOCH": 13091,
  "BSTAR": 0.00063669,
  "MEAN_MOTION_DOT": 0.00040476,
  "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	HAMMER
Operator	Open Cosmos Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Mar 4, 2024HIGHvia 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/59148

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