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 59917U 26145.51794435 +.00000000 +00000-0 +14298-3 0 00007
2 59917 97.5840 160.7403 0011903 312.0200 48.0019 15.16942576 07
| Epoch (UTC): | 25 May 2026 12:25:50 |
| Eccentricity: | 0.0011903 |
| inclination: | 97.5840° |
| perigee height: | 507 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 160.7403° |
| argument of perigee: | 312.0200° |
| revolutions per day: | 15.16942576 |
| mean anomaly at epoch: | 48.0019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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