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LEMUR-2 CARROLLEMO, 68489

Orbit data source: Space-Track

LEMUR-2 CARROLLEMO, 68489 is a payload satellite owned by Spire (DE) in SSO that was launched on Mon, 30 Mar 2026 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/68489?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

68489, 2026-067CB

Orbit

SSO

Country

DE / GER

Related business

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Com/MetRO

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

7.6 kg wet, 7.6 kg dry

Launch date (UTC)

2026-03-30 (4 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.3 m

Radar Cross Section

0.063 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 LEMUR-2 CARROLLEMO
1 68489U 26067CB  26220.11624818  .00001390  00000-0  14290-3 0  9991
2 68489  97.7566 177.4387 0000337 209.5302 150.5898 14.91934218 19466

Epoch: 2026-08-08T02:47Z

TLE epoch observation values (Epoch: 2026-08-08T02:47:23.842Z)

Latitude

-0.00003°

Longitude

178.95715°

Altitude

595.152 km

Speed

7.562 km/s

True Right ascension

11h 49m 45s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

23:59:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

589.158 km

Perigee altitude

588.689 km

Semi-major axis

6,967.06 km

Eccentricity

0.00003

Inclination

97.7566°

RAAN

177.4387°

Arg. of periapsis

209.5302°

True anomaly

150.5917°

Mean anomaly

150.5898°

Eccentric anomaly

150.59075°

Mean motion

3.73223 °/min

Orbital period

96.46 mins

BSTAR

0.0001429

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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)

LEMUR-2 CLARA, 68483

FGN-100-D3, 68464

HAWK-14C, 68441

IRIDE-MS1-EAG2-9, 68449

ICEYE-X73, 68496

LEMUR-2 EMARCHIA, 68492

OBJECT AT, 68457

OBJECT BD, 68467

OBJECT CP, 68501

AISSAT 4, 68454

VINDLER 2.1, 68488

OBJECT BP, 68477

IRIDE-MS1-EAG2-13, 68450

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 CARROLLEMO 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.
6 mins	2026-08-08 20:38:44.715Z	123.268° SE	2026-08-08 20:40:44.715Z	81.383° E	28.432°	2026-08-08 20:44:44.715Z	7.41° NNE

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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 CARROLLEMO, 68489 on other resources

View LEMUR-2 CARROLLEMO, 68489 on NASA - NSSDCA Website

View LEMUR-2 CARROLLEMO, 68489 on Heavens-Above

View LEMUR-2 CARROLLEMO, 68489 on Keep Track

View LEMUR-2 CARROLLEMO, 68489 on Celestrak

View LEMUR-2 CARROLLEMO, 68489 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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