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 10703U 78026B 23082.89100436 .00000001 00000-0 32056-4 0 9991
2 10703 99.1935 48.7343 0005685 286.0471 138.0006 13.99373396299078
| Epoch (UTC): | 23 March 2023 21:23:02 |
| Eccentricity: | 0.0005685 |
| inclination: | 99.1935° |
| perigee height: | 892 km |
| apogee height: | 900 km |
| right ascension of ascending node: | 48.7343° |
| argument of perigee: | 286.0471° |
| revolutions per day: | 13.99373396 |
| mean anomaly at epoch: | 138.0006° |
| orbit number at epoch: | 29907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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