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 39026U 12072A 23150.52106667 .00076273 00000-0 78189-3 0 9997
2 39026 97.2792 147.3613 0012895 346.6011 13.4904 15.64618609582595
| Epoch (UTC): | 30 May 2023 12:30:20 |
| Eccentricity: | 0.0012895 |
| inclination: | 97.2792° |
| perigee height: | 365 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 147.3613° |
| argument of perigee: | 346.6011° |
| revolutions per day: | 15.64618609 |
| mean anomaly at epoch: | 13.4904° |
| orbit number at epoch: | 58259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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