NOAA 16, 26536
Orbit data source: Space-Track
NOAA 16, 26536 is a payload satellite owned by NOAA (US) in SSO that was launched on Thu, 21 Sep 2000 UTC via a TITAN II SLV 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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26536 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LM/EW
Mission
Non-operational Civil Weather
Bus & Motor
ATN, Unknown motor
Mass
2,231 kg wet, 1,403 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 3.5 m
Radar Cross Section
11.218 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NOAA 16
1 26536U 00055A 26305.30733632 .00000033 00000-0 38733-4 0 9999
2 26536 98.4628 312.3548 0009308 267.3808 92.6301 14.13942692643107Epoch: 2026-11-01T07:22Z
TLE epoch observation values (Epoch: 2026-11-01T07:22:33.858Z)
Latitude
0.00006°
Longitude
161.11313°
Altitude
849.14 km
Speed
7.428 km/s
True Right ascension
20h 49m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:22:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
849.788 km
Perigee altitude
836.345 km
Semi-major axis
7,221.203 km
Eccentricity
0.00093
Inclination
98.4628°
RAAN
312.3548°
Arg. of periapsis
267.3808°
True anomaly
92.73664°
Mean anomaly
92.6301°
Eccentric anomaly
92.68337°
Mean motion
3.53695 °/min
Orbital period
101.78 mins
BSTAR
0.000038733
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Other satellites on launch #55 in the year 2000 (2000-09-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NOAA 16 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-02 00:29:21.579Z | 159.742° S | 2026-11-02 00:33:21.579Z | 29.909° NE | 76.932° | 2026-11-02 00:38:21.579Z | 349.183° N |
| 8 mins | 2026-11-02 12:51:21.579Z | 38.835° NE | 2026-11-02 12:54:21.579Z | 85.188° E | 38.063° | 2026-11-02 12:59:21.579Z | 163.094° S |
| 7 mins | 2026-11-02 14:32:21.579Z | 337.436° NNW | 2026-11-02 14:35:21.579Z | 292.129° WNW | 27.675° | 2026-11-02 14:39:21.579Z | 240.414° WSW |
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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