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 00059U 60013B 23026.08405424 .00000179 00000-0 12351-3 0 9996
2 00059 28.2507 4.6514 0189078 2.0940 358.0368 13.53016134 75358
| Epoch (UTC): | 26 January 2023 02:01:02 |
| Eccentricity: | 0.0189078 |
| inclination: | 28.2507° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 4.6514° |
| argument of perigee: | 2.0940° |
| revolutions per day: | 13.53016134 |
| mean anomaly at epoch: | 358.0368° |
| orbit number at epoch: | 7535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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