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SUOMI NPP

In orbit NORAD 37849 BSDY-9100-4436-7608-6479 United States of America

2011

Launch

0

Observations all time

Mission information
Spacecraft name
SUOMI NPP
Other names
2011-061A
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
2011-10-28 00:00:00
Separation time
2011-10-28 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
822.70 km
Apogee
825.46 km
Inclination
98.8°
Period
101.4 min
Semi-major axis
7202.2 km
Velocity
7.43 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:01 UTC
Two-line elements (TLE)
1 37849U 11061A   26286.89723412  .00000071  00000-0  54620-4 0  9999
2 37849 98.8056 227.0044 0001899 19.7528 340.3721 14.19538548775284
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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 12:55:01 SUOMI NPP
NORAD 37849
COSMOS 2251 DEB
NORAD 34790
4.824 14.83 6.5e-08
2026-10-14 14:36:18 SUOMI NPP
NORAD 37849
COSMOS 2251 DEB
NORAD 34790
0.941 14.83 1.7e-06
2026-10-14 21:35:56 SUOMI NPP
NORAD 37849
FENGYUN 1C DEB
NORAD 30570
4.216 10.37 1.9e-07
2026-10-15 04:26:35 SUOMI NPP
NORAD 37849
FENGYUN 1C DEB
NORAD 31085
3.141 9.89 3.5e-07
2026-10-15 05:11:46 SUOMI NPP
NORAD 37849
SL-3 R/B
NORAD 12646
3.849 9.00 6.7e-07
2026-10-15 09:33:35 SUOMI NPP
NORAD 37849
SL-16 DEB
NORAD 22370
4.389 12.66 1.4e-07
2026-10-16 00:33:16 SUOMI NPP
NORAD 37849
THOR ABLESTAR DEB
NORAD 3744
3.351 7.67 3.4e-07
2026-10-16 03:13:56 SUOMI NPP
NORAD 37849
FENGYUN 1C DEB
NORAD 36678
4.810 4.72 1.8e-07
2026-10-16 10:50:22 SUOMI NPP
NORAD 37849
FENGYUN 3D
NORAD 43010
2.803 4.62 5.4e-07
2026-10-16 10:50:39 SUOMI NPP
NORAD 37849
CZ-6A DEB
NORAD 54511
3.042 3.26 4.7e-07
2026-10-16 11:41:07 SUOMI NPP
NORAD 37849
FENGYUN 3D
NORAD 43010
0.834 4.61 6.1e-06
2026-10-16 15:01:45 SUOMI NPP
NORAD 37849
COSMOS 1275 DEB
NORAD 13022
3.411 8.18 3.2e-07
2026-10-16 16:44:45 SUOMI NPP
NORAD 37849
DMSP 5D-2 F13 DEB
NORAD 40412
2.253 8.70 7.3e-07
2026-10-17 05:25:51 SUOMI NPP
NORAD 37849
FENGYUN 1C DEB
NORAD 30377
3.831 9.00 2.5e-07
2026-10-17 07:07:42 MOST
NORAD 27843
SUOMI NPP
NORAD 37849
1.631 8.00 1.4e-06
2026-10-17 11:18:16 SUOMI NPP
NORAD 37849
COSMOS 2251 DEB
NORAD 35966
2.350 14.31 3.3e-07
2026-10-18 06:48:33 SUOMI NPP
NORAD 37849
CZ-6A DEB
NORAD 56635
4.956 8.37 1.5e-07
2026-10-18 16:11:01 SUOMI NPP
NORAD 37849
SL-14 DEB
NORAD 25204
3.276 14.84 1.4e-07
2026-10-18 23:43:21 SUOMI NPP
NORAD 37849
CZ-6A DEB
NORAD 54273
1.252 8.95 2.3e-06
2026-10-19 03:07:05 SUOMI NPP
NORAD 37849
COSMOS 1275 DEB
NORAD 42200
2.654 14.69 2.3e-07
2026-10-19 10:41:13 SUOMI NPP
NORAD 37849
NOAA 16 DEB
NORAD 41511
4.744 12.34 1.2e-07
2026-10-19 20:38:19 SUOMI NPP
NORAD 37849
FENGYUN 1C DEB
NORAD 30289
4.975 14.59 6.7e-08
2026-10-20 09:34:25 SUOMI NPP
NORAD 37849
METEOR 2-17 DEB
NORAD 28989
1.907 13.34 6.5e-07

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