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DELFI-N3XT

In orbit NORAD 39428 LDFA-5547-3453-6167-7352 Netherlands

2013

Launch

48

Observations all time

Mission information
Spacecraft name
DELFI-N3XT
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
2013-11-21 00:00:00
Separation time
Last observers
Observer
Time of receipt
2025-07-10 07:01:28 UTC
2025-07-10 02:25:33 UTC
2025-07-10 00:53:52 UTC
2025-07-08 09:53:11 UTC
2025-07-06 09:31:20 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
525.33 km
Apogee
625.58 km
Inclination
97.8°
Period
96.2 min
Semi-major axis
6953.6 km
Velocity
7.59 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:42 UTC
Two-line elements (TLE)
1 39428U 13066N   26280.77050921  .00003219  00000-0  27590-3 0  9992
2 39428 97.8301 201.0462 0072082 190.6958 169.2734 14.96268735691456
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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
2026-10-11 04:24:12 KUIPER-00179
NORAD 67136
DELFI-N3XT
NORAD 39428
3.200 6.03 4.0e-07
2026-10-12 07:41:45 KUIPER-00272
NORAD 68588
DELFI-N3XT
NORAD 39428
3.840 14.50 1.3e-07
2026-10-12 10:16:49 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
DELFI-N3XT
NORAD 39428
3.139 14.74 1.8e-07
2026-10-13 23:41:31 KUIPER-00600
NORAD 69284
DELFI-N3XT
NORAD 39428
2.318 6.06 7.6e-07
2026-10-14 02:25:06 ICEYE-X43
NORAD 60539
DELFI-N3XT
NORAD 39428
4.094 14.65 1.1e-07
2026-10-14 14:02:25 GEESAT-3 07
NORAD 61017
DELFI-N3XT
NORAD 39428
4.913 7.64 1.6e-07
2026-10-14 21:38:50 LEMUR-2-STAR-FOX
NORAD 62696
DELFI-N3XT
NORAD 39428
0.820 14.80 2.6e-06
2026-10-15 15:16:49 GEESAT-2 06
NORAD 58910
DELFI-N3XT
NORAD 39428
4.921 13.28 1.0e-07
2026-10-16 09:07:53 LEMUR-2-DELOITTE-5
NORAD 69910
DELFI-N3XT
NORAD 39428
3.782 2.80 3.0e-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