RU | EN | ZH --:-- UTC Sign in

NeonSat-1

In orbit NORAD 59587 EJOF-3230-5676-4528-8529 South Korea

2024

Launch

0

Observations all time

Mission information
Spacecraft name
NeonSat-1
Other names
New-space Earth Observation Satellite-1
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
2024-04-23 21:30:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
434.89 km
Apogee
444.20 km
Inclination
97.3°
Period
93.4 min
Semi-major axis
6817.6 km
Velocity
7.63 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:03 UTC
Two-line elements (TLE)
1 59587U 24077A   26287.25616826  .00015435  00000-0  37327-3 0  9998
2 59587 97.3429 11.7144 0006772 330.4434 29.6429 15.41207193138053
Copy content
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
2026-10-15 13:48:03 NEONSAT-1
NORAD 59587
TAURUS R/B
NORAD 26103
3.276 14.51 2.4e-07
2026-10-16 00:46:00 NEONSAT-1
NORAD 59587
STARLINK-37751
NORAD 100491
1.932 12.48 2.3e-05
2026-10-16 05:14:55 DONGPO 09
NORAD 54685
NEONSAT-1
NORAD 59587
4.488 10.93 1.6e-07
2026-10-16 11:30:19 OBJECT AS
NORAD 57044
NEONSAT-1
NORAD 59587
4.059 4.14 2.6e-07
2026-10-17 22:45:51 STARLINK-4485
NORAD 53541
NEONSAT-1
NORAD 59587
2.638 13.93 9.8e-06
2026-10-17 22:51:34 NEONSAT-1
NORAD 59587
COSMOS 1220 DEB
NORAD 25795
4.505 4.67 2.1e-07
2026-10-18 00:19:18 STARLINK-4485
NORAD 53541
NEONSAT-1
NORAD 59587
3.123 13.91 7.0e-06
2026-10-18 01:52:45 STARLINK-4485
NORAD 53541
NEONSAT-1
NORAD 59587
3.385 13.90 6.0e-06
2026-10-18 03:26:11 STARLINK-4485
NORAD 53541
NEONSAT-1
NORAD 59587
1.894 13.88 1.9e-05
2026-10-18 04:59:37 STARLINK-4485
NORAD 53541
NEONSAT-1
NORAD 59587
2.241 13.87 1.4e-05
2026-10-18 07:53:14 LEMUR-2-ANDIS
NORAD 42838
NEONSAT-1
NORAD 59587
3.484 11.31 2.6e-07
2026-10-19 03:37:21 STARLINK-5593
NORAD 55763
NEONSAT-1
NORAD 59587
3.131 4.60 1.3e-05
2026-10-19 17:54:37 STARLINK-3225
NORAD 49737
NEONSAT-1
NORAD 59587
4.762 14.67 2.5e-06
2026-10-19 18:41:20 STARLINK-3225
NORAD 49737
NEONSAT-1
NORAD 59587
3.382 14.69 5.0e-06

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