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 61913U 26145.22539748 +.00000000 +00000-0 +83965-3 0 00005
2 61913 43.0031 209.8248 0001106 269.3946 90.6779 15.27630647 02
| Epoch (UTC): | 25 May 2026 05:24:34 |
| Eccentricity: | 0.0001106 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.8248° |
| argument of perigee: | 269.3946° |
| revolutions per day: | 15.27630647 |
| mean anomaly at epoch: | 90.6779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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