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 00115U 60002D 25173.08296244 .00002250 00000-0 22340-3 0 9991
2 00115 48.1633 68.4534 0027184 78.5261 281.8706 14.95150428464190
| Epoch (UTC): | 22 June 2025 01:59:27 |
| Eccentricity: | 0.0027184 |
| inclination: | 48.1633° |
| perigee height: | 563 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 68.4534° |
| argument of perigee: | 78.5261° |
| revolutions per day: | 14.95150428 |
| mean anomaly at epoch: | 281.8706° |
| orbit number at epoch: | 46419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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