View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64154U 26145.40395295 +.00000000 +00000-0 +36843-3 0 00005
2 64154 97.4473 205.2770 0001984 144.7677 215.3682 15.05653939 00
| Epoch (UTC): | 25 May 2026 09:41:41 |
| Eccentricity: | 0.0001984 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.2770° |
| argument of perigee: | 144.7677° |
| revolutions per day: | 15.05653939 |
| mean anomaly at epoch: | 215.3682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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