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

VIREON-1

In orbit NORAD 68434 AOCK-4566-1105-2287-8628

Observations 0
Go to map
Back

2026

Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
VIREON-1
Other names
CYCLOPS-1, ACC-CYCLOPS
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
504.67 km
Apogee
505.73 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6883.3 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 68434U 26067U   26282.94847106  .00002571  00000-0  12541-3 0  9996
2 68434  97.4735 240.0992 0000772  32.5097 327.6185 15.19209090 29368
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
2026-10-12 04:51:12 OBJECT Z
NORAD 67271 		VIREON-1
NORAD 68434 		3.710 12.75 2.0e-07
2026-10-12 08:43:02 FOSSASAT-2E21
NORAD 64536 		VIREON-1
NORAD 68434 		2.447 14.73 3.0e-07
2026-10-13 05:21:23 FOSSASAT-2E22
NORAD 66779 		VIREON-1
NORAD 68434 		4.256 12.62 1.5e-07
2026-10-13 06:56:13 FOSSASAT-2E22
NORAD 66779 		VIREON-1
NORAD 68434 		4.075 12.62 1.7e-07
2026-10-14 18:32:20 SUPERVIEW NEO-2 04
NORAD 62080 		VIREON-1
NORAD 68434 		2.173 6.20 8.6e-07
2026-10-14 18:32:20 SUPERVIEW NEO-2 03
NORAD 62079 		VIREON-1
NORAD 68434 		2.336 6.20 7.5e-07
2026-10-14 19:19:46 SUPERVIEW NEO-2 04
NORAD 62080 		VIREON-1
NORAD 68434 		3.545 6.19 3.2e-07
2026-10-14 19:19:46 SUPERVIEW NEO-2 03
NORAD 62079 		VIREON-1
NORAD 68434 		2.114 6.19 9.1e-07
2026-10-15 07:08:57 OBJECT AB
NORAD 67273 		VIREON-1
NORAD 68434 		3.824 12.74 1.9e-07
2026-10-15 10:19:27 ION SCV-013
NORAD 58300 		VIREON-1
NORAD 68434 		4.945 11.26 1.3e-07
2026-10-15 11:52:55 COSMOS 2538
NORAD 44424 		VIREON-1
NORAD 68434 		4.886 13.26 1.1e-07
2026-10-15 19:50:04 VIREON-1
NORAD 68434 		UNKNOWN
NORAD 81969 		4.095 13.98 1.3e-07
2026-10-16 10:03:33 HJ-2E
NORAD 54035 		VIREON-1
NORAD 68434 		1.570 5.78 1.7e-06
2026-10-17 05:33:48 VIREON-1
NORAD 68434 		UNISAT
NORAD 26547 		2.428 14.97 1.0e-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