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 25407U 98045B 23153.08220013 .00000143 00000-0 96726-4 0 9996
2 25407 71.0097 148.4849 0005900 140.8623 219.2928 14.15917097284168
| Epoch (UTC): | 02 June 2023 01:58:22 |
| Eccentricity: | 0.0005900 |
| inclination: | 71.0097° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 148.4849° |
| argument of perigee: | 140.8623° |
| revolutions per day: | 14.15917097 |
| mean anomaly at epoch: | 219.2928° |
| orbit number at epoch: | 28416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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