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 64013U 26145.39969252 +.00000000 +00000-0 +64764-3 0 00000
2 64013 42.9986 281.5740 0000579 216.6301 143.4511 15.27605024 02
| Epoch (UTC): | 25 May 2026 09:35:33 |
| Eccentricity: | 0.0000579 |
| inclination: | 42.9986° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 281.5740° |
| argument of perigee: | 216.6301° |
| revolutions per day: | 15.27605024 |
| mean anomaly at epoch: | 143.4511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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