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ELEMENT-1

In orbit NORAD 100901 UNFM-4607-8123-7880-9625

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ELEMENT-1
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
Apogee
Inclination
97.4°
Period
94.9 min
Semi-major axis
6888.1 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 14:09:06 UTC
Two-line elements (TLE)
1 A0901U 26227U   26286.15576603  .00013092  00000-0  65349-3 0  9991
2 A0901 97.4424 355.4766 0003434 106.2334 253.9278 15.17622529 1738
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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 01:32:39 DB-PFW
NORAD 68466
ELEMENT-1
NORAD 100901
2.659 12.53 3.9e-07
2026-10-15 00:08:47 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BA
NORAD 100931
2.218 0.00 7.6e-06
2026-10-15 01:18:51 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BA
NORAD 100931
0.763 0.00 7.6e-06
2026-10-15 02:06:42 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BA
NORAD 100931
0.756 0.00 7.6e-06
2026-10-15 03:44:21 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BA
NORAD 100931
3.971 0.01 7.6e-06
2026-10-15 12:47:29 ELEMENT-1
NORAD 100901
ION SCV-025
NORAD 100925
0.586 0.00 6.8e-06
2026-10-15 22:42:38 ELEMENT-1
NORAD 100901
UNKNOWN
NORAD 82180
3.852 14.08 1.5e-07
2026-10-16 22:40:54 ELEMENT-1
NORAD 100901
INMARSAT 2-F2 R/B(PAM-D)
NORAD 21151
2.868 10.24 5.8e-07
2026-10-17 16:32:47 TIANHUI 2-02A
NORAD 49071
ELEMENT-1
NORAD 100901
2.594 8.37 5.6e-07
2026-10-17 16:32:47 TIANHUI 2-02B
NORAD 49072
ELEMENT-1
NORAD 100901
2.897 8.37 4.5e-07
2026-10-17 17:51:46 YAOGAN-39 03C
NORAD 57990
ELEMENT-1
NORAD 100901
3.087 12.14 3.0e-07
2026-10-17 18:55:04 TERRASAR-X
NORAD 31698
ELEMENT-1
NORAD 100901
4.491 7.92 1.9e-07
2026-10-17 18:55:04 TANDEM-X
NORAD 36605
ELEMENT-1
NORAD 100901
3.286 7.92 3.6e-07
2026-10-18 03:18:39 ELEMENT-1
NORAD 100901
QAEM 100 R/B
NORAD 61071
2.288 4.79 8.1e-07
2026-10-18 09:47:37 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BF
NORAD 100936
2.146 0.00 1.0e-05
2026-10-18 10:59:54 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BF
NORAD 100936
1.064 0.00 1.0e-05
2026-10-18 11:55:52 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BF
NORAD 100936
0.649 0.00 1.0e-05
2026-10-18 13:30:09 ELEMENT-1
NORAD 100901
TRANSPORTER-18 OBJECT BF
NORAD 100936
4.047 0.01 2.7e-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