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NOAA 18

In orbit NORAD 28654 SWSC-0362-2710-3817-5254 United States of America

2005

Launch

16135

Observations all time

American weather satellite

Mission description
Mission information
Spacecraft name
NOAA 18
Mass
2232.0 kg
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2005-05-20 00:00:00
Separation time
Last observers
Observer
Time of receipt
2025-06-29 20:59:20 UTC
2025-06-29 19:15:04 UTC
Satellite appearance

Credit: Credit: NOAA NESDIS Environmental Visualization Laboratory. Public domain source

Orbital parameters of the satellite
Perigee
833.51 km
Apogee
853.99 km
Inclination
98.8°
Period
101.9 min
Semi-major axis
7221.9 km
Velocity
7.43 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:42 UTC
Two-line elements (TLE)
1 28654U 05018A   26280.93575726  .00000025  00000-0  36324-4 0  9990
2 28654 98.8039 358.9331 0014184 186.3388 173.7607 14.13746502102244
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-14 20:32:52 YAOGAN-40 01B
NORAD 57832
NOAA 18
NORAD 28654
3.403 14.58 1.4e-07
2026-10-14 22:14:50 YAOGAN-40 01B
NORAD 57832
NOAA 18
NORAD 28654
2.478 14.58 2.7e-07
2026-10-15 03:20:37 YAOGAN-40 01A
NORAD 57830
NOAA 18
NORAD 28654
1.431 14.58 8.1e-07
2026-10-15 05:02:35 YAOGAN-40 01A
NORAD 57830
NOAA 18
NORAD 28654
4.524 14.59 8.0e-08
2026-10-15 06:44:37 YAOGAN-40 01C
NORAD 57833
NOAA 18
NORAD 28654
4.889 14.60 6.8e-08
2026-10-15 08:26:35 YAOGAN-40 01C
NORAD 57833
NOAA 18
NORAD 28654
1.709 14.61 5.6e-07
2026-10-15 10:08:33 YAOGAN-40 01C
NORAD 57833
NOAA 18
NORAD 28654
4.298 14.61 8.8e-08

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite