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PIXL-1

In orbit NORAD 47448 HGYE-7318-8290-9065-4147 Germany

Time in UTC

00:06

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 23°

—

No observations scheduled

1

Observations over 30 days

91%

Successful observations

96k

Frames, latest 2026-09-29 00:49 UTC

Mission information
Spacecraft name
PIXL-1
Other names
CubeL, OSIRIS4CubeSat
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 40
Launch time
2021-01-24 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-02-10 17:16:10 UTC
2026-02-07 06:50:50 UTC
2026-02-06 07:24:47 UTC
2026-02-05 06:27:31 UTC
2025-06-17 10:03:03 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
423.57 km
Apogee
434.01 km
Inclination
97.2°
Period
93.2 min
Semi-major axis
6806.9 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 47448U 21006AM  26283.40238725  .00020302  00000-0  43364-3 0  9998
2 47448 97.2191 333.0965 0007677 112.3501 247.8562 15.44851924317522
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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 13:23:43 CUBEL
NORAD 47448
SL-8 DEB
NORAD 1392
3.674 12.40 2.1e-07
2026-10-12 01:56:43 STARLINK-1443
NORAD 45660
CUBEL
NORAD 47448
1.919 14.56 1.6e-05
2026-10-12 06:53:01 CUBEL
NORAD 47448
OBJECT A
NORAD 56731
2.797 13.52 3.1e-07
2026-10-14 01:42:49 CUBEL
NORAD 47448
R5-S4
NORAD 60206
1.832 14.94 5.1e-07
2026-10-15 00:55:47 CUBEL
NORAD 47448
PSLV R/B
NORAD 46915
4.000 13.32 1.6e-07
2026-10-15 15:10:05 CUBEL
NORAD 47448
FLOCK 4BE-25
NORAD 60487
3.574 4.49 3.3e-07
2026-10-15 18:07:10 CUBEL
NORAD 47448
LEMUR-2-VALHALLA
NORAD 58900
4.343 14.96 9.0e-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