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 data is extracted from the following two-line orbital elements,
1 28095U 03054A 23086.80748667 0.00000300 00000-0 26130-3 0 02
2 28095 63.4024 316.4504 0493056 1.9093 358.0907 13.41504790 03
| Epoch (UTC): | 27 March 2023 19:22:46 |
| Eccentricity: | 0.0493056 |
| inclination: | 63.4024° |
| perigee height: | 735 km |
| apogee height: | 1472 km |
| right ascension of ascending node: | 316.4504° |
| argument of perigee: | 1.9093° |
| revolutions per day: | 13.41504790 |
| mean anomaly at epoch: | 358.0907° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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