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 27844U 03031E 23080.76360237 .00000604 00000-0 28897-3 0 9996
2 27844 98.6811 89.2948 0010267 25.6513 334.5173 14.22687856 23301
| Epoch (UTC): | 21 March 2023 18:19:35 |
| Eccentricity: | 0.0010267 |
| inclination: | 98.6811° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 89.2948° |
| argument of perigee: | 25.6513° |
| revolutions per day: | 14.22687856 |
| mean anomaly at epoch: | 334.5173° |
| orbit number at epoch: | 2330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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