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THEMIS E, 30798

Orbit data source: Space-Track

THEMIS E, 30798 is a payload satellite owned by GSFC (US) in HEO that was launched on Sat, 17 Feb 2007 UTC via a DELTA 7925-10C launch vehicle from the Air Force Eastern Test Range (AFETR). 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/30798?theme=dark&initialShowStats=false

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Identifier

30798, 2007-004E

Orbit

HEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Swales

Mission

Operational Civil Science

Bus & Motor

ATK-A100, Unknown motor

Mass

125 kg wet, 76 kg dry

Launch date (UTC)

2007-02-17 (19 years ago)

Launch vehicle

DELTA 7925-10C

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 6 Rod, 24.5 m

Radar Cross Section

0.720 m², Medium (>0.1 m² and < 1m²)

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

TLE from 2 days ago

0 THEMIS E
1 30798U 07004E   26119.63846429 -.00000032  00000-0  00000-0 0  9995
2 30798   5.7674 100.9635 8447478 206.8239 183.8447  0.88331981 65494

Epoch: 2026-04-29T15:19Z

TLE epoch observation values (Epoch: 2026-04-29T15:19:23.314Z)

Latitude

2.64563°

Longitude

40.86451°

Altitude

78,111.417 km

Speed

0.865 km/s

True Right ascension

08h 33m 13s

True Declination

2° 38' 39"

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

14:53:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

78,276.777 km

Perigee altitude

746.339 km

Semi-major axis

45,889.695 km

Eccentricity

0.84475

Inclination

5.7674°

RAAN

100.9635°

Arg. of periapsis

206.8239°

True anomaly

180.60473°

Mean anomaly

183.8447°

Eccentric anomaly

182.08434°

Mean motion

0.22079 °/min

Orbital period

1,630.54 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #4 in the year 2007 (2007-02-17 UTC)

THEMIS A, 30580

THEMIS D, 30797

DELTA 2 R/B(1), 30585 (Decayed)

ARTEMIS P2 (THEMIS C), 30582

DELTA 2 R/B(2), 30799 (Decayed)

ARTEMIS P1 (THEMIS B), 30581

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THEMIS E 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.
13 mins	2026-05-01 07:17:01.527Z	189.793° SSW	2026-05-01 07:17:01.527Z	189.793° SSW	27.001°	2026-05-01 07:30:01.527Z	154.718° SSE
688 mins	2026-05-01 19:49:01.527Z	99.42° ESE	2026-05-02 01:30:01.527Z	180.568° SSW	37.677°	2026-05-02 07:17:01.527Z	258.598° W

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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 THEMIS E, 30798 on other resources

View THEMIS E, 30798 on NASA - NSSDCA Website

View THEMIS E, 30798 on Heavens-Above

View THEMIS E, 30798 on Keep Track

View THEMIS E, 30798 on Celestrak

View THEMIS E, 30798 on Gunter's Space Page

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

THEMIS E, 30798

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: 2026-04-29T15:19:23.314Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #4 in the year 2007 (2007-02-17 UTC)

THEMIS E Visibility forecast

Co-orbital & Co-planar RSOs

Check out THEMIS E, 30798 on other resources

Documentation

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