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VINDLER 2.2, 68484

Orbit data source: Space-Track

VINDLER 2.2, 68484 is an American payload satellite 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/68484?theme=dark&initialShowStats=false

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Identifier

68484, 2026-067BW

Orbit

SSO

Country

Related business

None

Manufacturer

Unknown

Mission

Operational spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2026-03-30 (1 month ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 1.1 m

Radar Cross Section

RCS unknown

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 VINDLER 2.2
1 68484U 26067BW  26125.44903512  .00001418  00000-0  14363-3 0  9999
2 68484  97.7595  84.3924 0003048  87.3384 272.8184 14.92493482  5353

Epoch: 2026-05-05T10:46Z

TLE epoch observation values (Epoch: 2026-05-05T10:46:36.634Z)

Latitude

-0.00002°

Longitude

59.41604°

Altitude

593.103 km

Speed

7.563 km/s

True Right ascension

05h 37m 34s

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

01:02:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

589.305 km

Perigee altitude

585.059 km

Semi-major axis

6,965.319 km

Eccentricity

0.0003

Inclination

97.7595°

RAAN

84.3924°

Arg. of periapsis

87.3384°

True anomaly

272.78351°

Mean anomaly

272.8184°

Eccentric anomaly

272.80096°

Mean motion

3.73363 °/min

Orbital period

96.42 mins

BSTAR

0.00014363

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

LEMUR-2 EMARCHIA, 68492

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VINDLER 2.2 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.
7 mins	2026-05-07 20:49:39.706Z	143.464° SSE	2026-05-07 20:53:39.706Z	55.167° ENE	34.216°	2026-05-07 20:56:39.706Z	3.478° NNE
6 mins	2026-05-08 10:09:39.706Z	11.502° NNE	2026-05-08 10:11:39.706Z	358.666° N	44.662°	2026-05-08 10:15:39.706Z	194.442° SSW

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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 VINDLER 2.2, 68484 on other resources

View VINDLER 2.2, 68484 on NASA - NSSDCA Website

View VINDLER 2.2, 68484 on Heavens-Above

View VINDLER 2.2, 68484 on Keep Track

View VINDLER 2.2, 68484 on Celestrak

View VINDLER 2.2, 68484 on Gunter's Space Page

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

VINDLER 2.2, 68484

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-05-05T10:46:36.634Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

VINDLER 2.2 Visibility forecast

Co-orbital & Co-planar RSOs

Check out VINDLER 2.2, 68484 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago