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 68573U 26145.39971802 +.00000000 +00000-0 +13860-2 0 00009
2 68573 51.8988 296.4141 0001542 131.7064 228.4031 14.79949339 09
| Epoch (UTC): | 25 May 2026 09:35:35 |
| Eccentricity: | 0.0001542 |
| inclination: | 51.8988° |
| perigee height: | 628 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 296.4141° |
| argument of perigee: | 131.7064° |
| revolutions per day: | 14.79949339 |
| mean anomaly at epoch: | 228.4031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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