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 59704U 26145.54407977 +.00000000 +00000-0 -10496-3 0 00003
2 59704 43.0031 346.0692 0000665 288.3609 71.7170 15.27597432 09
| Epoch (UTC): | 25 May 2026 13:03:28 |
| Eccentricity: | 0.0000665 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 346.0692° |
| argument of perigee: | 288.3609° |
| revolutions per day: | 15.27597432 |
| mean anomaly at epoch: | 71.7170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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