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 58021U 26145.18300483 +.00000000 +00000-0 +39380-3 0 00000
2 58021 97.5427 221.7974 0003650 329.8212 30.2813 15.21323535 02
| Epoch (UTC): | 25 May 2026 04:23:31 |
| Eccentricity: | 0.0003650 |
| inclination: | 97.5427° |
| perigee height: | 499 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 221.7974° |
| argument of perigee: | 329.8212° |
| revolutions per day: | 15.21323535 |
| mean anomaly at epoch: | 30.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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