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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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https://www.satcat.com/sats-embedded/59146?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59146, 2024-043BA

Orbit

SSO

Country

US

Related business

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Communications

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

22 kg wet, 22 kg dry

Launch date (UTC)

2024-03-04 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 4 Pan, 1.4 m

Radar Cross Section

0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  26254.41135909  .00043588  00000-0  40673-3 0  9990
2 59146  97.5438  51.9326 0003381 216.0075 144.0958 15.67205791141511

Epoch: 2026-09-11T09:52Z

TLE epoch observation values (Epoch: 2026-09-11T09:52:21.425Z)

Latitude

-0°

Longitude

-86.59177°

Altitude

371.9 km

Speed

7.685 km/s

True Right ascension

03h 27m 43s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

14:54:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

366.091 km

Perigee altitude

361.532 km

Semi-major axis

6,741.949 km

Eccentricity

0.00034

Inclination

97.5438°

RAAN

51.9326°

Arg. of periapsis

216.0075°

True anomaly

144.11851°

Mean anomaly

144.0958°

Eccentric anomaly

144.10716°

Mean motion

3.92071 °/min

Orbital period

91.82 mins

BSTAR

0.00040673

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

LIZZIESAT, 59132

ICEYE-X38, 59100

OBJECT R, 59113 (Decayed)

SONATE-2, 59112

PE2_FLT2 (TYVAK-0262), 59104

OBJECT AT, 59139 (Decayed)

METHANESAT, 59101

NUSAT-44 MARIA MITCHELL, 59122

APEX ARIES 1, 59129

VSP RF A1, 59135

LYNK TOWER 6, 59123

OBJECT P, 59111 (Decayed)

LYNK TOWER 5, 59121

JACKAL-01, 59127

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

LEMUR 2 JOHNNYTRUONG Visibility forecast

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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	2026-09-12 10:31:56.065Z	154.501° SSE	2026-09-12 10:33:56.065Z	51.443° ENE	62.913°	2026-09-12 10:35:56.065Z	356.179° N

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out LEMUR 2 JOHNNYTRUONG, 59146 on other resources

View LEMUR 2 JOHNNYTRUONG, 59146 on NASA - NSSDCA Website

View LEMUR 2 JOHNNYTRUONG, 59146 on Heavens-Above

View LEMUR 2 JOHNNYTRUONG, 59146 on Keep Track

View LEMUR 2 JOHNNYTRUONG, 59146 on Celestrak

View LEMUR 2 JOHNNYTRUONG, 59146 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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