NOAA 17 DEB, 48614

Orbit data source: Space-Track

NOAA 17 DEB, 48614 is space debris in SSO originally from a launch on Mon, 24 Jun 2002 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Iframe URL

https://www.satcat.com/sats-embedded/48614?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

48614, 2002-032AF

Orbit

SSO

Last TLE update

1 day ago

Origin

National Oceanic and Atmospheric Administration (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2002-06-24 (23 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 NOAA 17 DEB
1 48614U 02032AF  25177.22920676  .00023800  00000-0  29942-2 0  9997
2 48614  98.6611 169.4345 0010611  48.5973 311.6148 14.82010949225936

Epoch: 2025-06-26T05:30Z

TLE epoch observation values (Epoch: 2025-06-26T05:30:03.464Z)

Latitude

-0°

Longitude

172.32064°

Altitude

621.054 km

Speed

7.551 km/s

True Right ascension

11h 17m 44s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-2.85051°

Longitude

174.06618°

Altitude

621.188 km

Speed

7.551 km/s

Apparent Right ascension

10h 50m 42s

Apparent Declination

-20° 40' 41"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

22:01:59

Azimuth

328.004° NNW

Elevation

-68.125°

Doppler factor

Orbital elements

Apogee altitude

627.483 km

Perigee altitude

612.632 km

Semi-major axis

6,998.195 km

Eccentricity

0.00106

Inclination

98.6611°

RAAN

169.4345°

Arg. of periapsis

48.5973°

True anomaly

Unknown

Mean anomaly

311.6148°

Eccentric anomaly

Unknown

Mean motion

3.70735 °/min

Orbital period

97.1 mins

BSTAR

0.0029942

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Other satellites on launch #32 in the year 2002 (2002-06-24 UTC)

NOAA 17, 27453

NOAA 17 DEB, 48185 (Decayed)

NOAA 17 DEB, 48186 (Decayed)

NOAA 17 DEB, 48611

NOAA 17 DEB, 48612 (Decayed)

NOAA 17 DEB, 48613 (Decayed)

NOAA 17 DEB, 48615

NOAA 17 DEB, 48616

NOAA 17 DEB, 48617 (Decayed)

NOAA 17 DEB, 48702

NOAA 17 DEB, 48703 (Decayed)

NOAA 17 DEB, 48704 (Decayed)

NOAA 17 DEB, 48705

NOAA 17 DEB, 48706

NOAA 17 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-06-27 11:16:16.182Z	64.717° ENE	2025-06-27 11:18:16.182Z	94.256° ESE	14.115°	2025-06-27 11:20:16.182Z	123.253° SE
6 mins	2025-06-27 12:52:16.182Z	348.86° N	2025-06-27 12:54:16.182Z	298.397° NW	35.757°	2025-06-27 12:58:16.182Z	216.584° SW
6 mins	2025-06-27 23:46:16.182Z	189.591° SSW	2025-06-27 23:48:16.182Z	245.569° WSW	39.672°	2025-06-27 23:52:16.182Z	336.568° NNW

Authenticating...

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Check out NOAA 17 DEB, 48614 on other resources

View NOAA 17 DEB, 48614 on Heavens-Above

View NOAA 17 DEB, 48614 on Keep Track

View NOAA 17 DEB, 48614 on Celestrak

View NOAA 17 DEB, 48614 on Gunter's Space Page

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