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 60315U 26145.45740323 +.00000000 +00000-0 +35302-4 0 00001
2 60315 53.1611 300.4954 0000984 78.2522 281.8589 15.30196617 06
| Epoch (UTC): | 25 May 2026 10:58:39 |
| Eccentricity: | 0.0000984 |
| inclination: | 53.1611° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.4954° |
| argument of perigee: | 78.2522° |
| revolutions per day: | 15.30196617 |
| mean anomaly at epoch: | 281.8589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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