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 27597U 02056A 23088.43264147 .00000851 00000-0 36178-3 0 9997
2 27597 98.6411 33.5314 0000223 80.7039 279.4167 14.27841086 56631
| Epoch (UTC): | 29 March 2023 10:23:00 |
| Eccentricity: | 0.0000223 |
| inclination: | 98.6411° |
| perigee height: | 799 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 33.5314° |
| argument of perigee: | 80.7039° |
| revolutions per day: | 14.27841086 |
| mean anomaly at epoch: | 279.4167° |
| orbit number at epoch: | 5663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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