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 is defined by the following mean orbital elements,
1 57828U 26145.47862713 +.00000000 +00000-0 +11832-4 0 00008
2 57828 43.0037 160.3699 0000998 278.4009 81.6729 15.27575611 02
| Epoch (UTC): | 25 May 2026 11:29:13 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.3699° |
| argument of perigee: | 278.4009° |
| revolutions per day: | 15.27575611 |
| mean anomaly at epoch: | 81.6729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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