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 25338U 98030A 23152.93432580 .00000269 00000-0 13020-3 0 9994
2 25338 98.6063 182.2514 0010302 5.5652 354.5641 14.26324955302832
| Epoch (UTC): | 01 June 2023 22:25:25 |
| Eccentricity: | 0.0010302 |
| inclination: | 98.6063° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 182.2514° |
| argument of perigee: | 5.5652° |
| revolutions per day: | 14.26324955 |
| mean anomaly at epoch: | 354.5641° |
| orbit number at epoch: | 30283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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