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 68759U 26145.75865169 +.00000000 +00000-0 +11209-3 0 00009
2 68759 97.8078 282.8739 0012662 132.0339 228.1968 15.06074395 09
| Epoch (UTC): | 25 May 2026 18:12:27 |
| Eccentricity: | 0.0012662 |
| inclination: | 97.8078° |
| perigee height: | 539 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 282.8739° |
| argument of perigee: | 132.0339° |
| revolutions per day: | 15.06074395 |
| mean anomaly at epoch: | 228.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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