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 25757U 26145.42182237 +.00000000 +00000-0 +32594-4 0 00003
2 25757 98.6692 140.1778 0015254 61.7953 298.4779 14.52419742 09
| Epoch (UTC): | 25 May 2026 10:07:25 |
| Eccentricity: | 0.0015254 |
| inclination: | 98.6692° |
| perigee height: | 707 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 140.1778° |
| argument of perigee: | 61.7953° |
| revolutions per day: | 14.52419742 |
| mean anomaly at epoch: | 298.4779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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