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 40981U 15058R 23050.75623831 0.00000000 00000-0 00000-0 0 09
2 40981 63.4367 284.5278 0104476 1.8453 358.1546 13.40861684 05
| Epoch (UTC): | 19 February 2023 18:08:58 |
| Eccentricity: | 0.0104476 |
| inclination: | 63.4367° |
| perigee height: | 1028 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 284.5278° |
| argument of perigee: | 1.8453° |
| revolutions per day: | 13.40861684 |
| mean anomaly at epoch: | 358.1546° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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