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HAMMER, 59148

Orbit data source: Space-Track

HAMMER, 59148 is a payload satellite owned by Open Cosmos (ES) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe URL

https://www.satcat.com/sats-embedded/59148?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59148, 2024-043BC

Orbit

SSO

Last TLE update

8 hours ago

Origin

Open Cosmos Ltd. (ES / SPN)

Manufacturer

Open Cosmos

Mission

Operational Commercial Com/MetRO

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

~10 kg wet, ~10 kg dry

Launch date (UTC)

2024-03-04 (1 year ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.5 m

Radar Cross Section

0.063 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 hours ago

0 HAMMER
1 59148U 24043BC  25199.62108561  .00008569  00000-0  24931-3 0  9995
2 59148  97.5122 332.4084 0007112 301.8623  58.1928 15.35663349 76385

Epoch: 2025-07-18T14:54Z

TLE epoch observation values (Epoch: 2025-07-18T14:54:21.796Z)

Latitude

-0°

Longitude

172.14766°

Altitude

459.498 km

Speed

7.638 km/s

True Right ascension

22h 09m 38s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

48.56983°

Longitude

1.04933°

Altitude

471.414 km

Speed

7.632 km/s

Apparent Right ascension

04h 36m 37s

Apparent Declination

31° 51' 18"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:05:13

Azimuth

307.803° NW

Elevation

5.338°

Doppler factor

Orbital elements

Apogee altitude

460.761 km

Perigee altitude

451.04 km

Semi-major axis

6,834.037 km

Eccentricity

0.00071

Inclination

97.5122°

RAAN

332.4084°

Arg. of periapsis

301.8623°

True anomaly

58.26209°

Mean anomaly

58.1928°

Eccentric anomaly

58.22744°

Mean motion

3.84173 °/min

Orbital period

93.71 mins

BSTAR

0.00024931

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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)

HORACIO, 59098

NUSAT-44 MARIA MITCHELL, 59122

HAMMER Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
4 mins	2025-07-19 08:15:38.643Z	114.83° SE	2025-07-19 08:17:38.643Z	67.644° E	22.012°	2025-07-19 08:19:38.643Z	23.708° NE
4 mins	2025-07-19 21:12:38.643Z	62.151° ENE	2025-07-19 21:13:38.643Z	90.567° ESE	24.825°	2025-07-19 21:16:38.643Z	156.164° SSE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Authenticating...

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Check out HAMMER, 59148 on other resources

View HAMMER, 59148 on NASA - NSSDCA Website

View HAMMER, 59148 on Heavens-Above

View HAMMER, 59148 on Keep Track

View HAMMER, 59148 on Celestrak

View HAMMER, 59148 on Gunter's Space Page

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