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LEMUR 2 JOHNNYTRUONG, 59146

Orbit data source: Space-Track

LEMUR 2 JOHNNYTRUONG, 59146 is an American payload satellite 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/59146?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59146, 2024-043BA

Orbit

SSO

Last TLE update

11 hours ago

Origin

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Civil Technology

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

22 kg wet, 22 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, 0.1 m

Radar Cross Section

0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 hours ago

0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  25228.32784766  .00015574  00000-0  39624-3 0  9999
2 59146  97.5105   1.9586 0006375 197.8539 162.2484 15.39666028 80838

Epoch: 2025-08-16T07:52Z

TLE epoch observation values (Epoch: 2025-08-16T07:52:06.037Z)

Latitude

0.00001°

Longitude

-81.03122°

Altitude

454.355 km

Speed

7.638 km/s

True Right ascension

00h 07m 50s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

28.79494°

Longitude

-84.69168°

Altitude

455.018 km

Speed

7.64 km/s

Apparent Right ascension

22h 51m 39s

Apparent Declination

-4° 22' 52"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

09:35:55

Azimuth

329.378° NNW

Elevation

-50.568°

Doppler factor

Orbital elements

Apogee altitude

448.389 km

Perigee altitude

439.691 km

Semi-major axis

6,822.177 km

Eccentricity

0.00064

Inclination

97.5105°

RAAN

1.9586°

Arg. of periapsis

197.8539°

True anomaly

162.27066°

Mean anomaly

162.2484°

Eccentric anomaly

162.25953°

Mean motion

3.85176 °/min

Orbital period

93.46 mins

BSTAR

0.00039624

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

HORACIO, 59098

NUSAT-44 MARIA MITCHELL, 59122

LEMUR 2 JOHNNYTRUONG Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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	2025-08-16 22:28:43.864Z	328.415° NNW	2025-08-16 22:29:43.864Z	303.35° NW	23.091°	2025-08-16 22:32:43.864Z	233.037° WSW
5 mins	2025-08-17 08:57:43.864Z	162.414° S	2025-08-17 08:59:43.864Z	134.313° SE	43.665°	2025-08-17 09:02:43.864Z	350.715° N