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 68843U 26145.49548028 +.00000000 +00000-0 +20543-2 0 00006
2 68843 97.2834 160.4557 0001524 56.5623 303.5787 15.75323714 02
| Epoch (UTC): | 25 May 2026 11:53:29 |
| Eccentricity: | 0.0001524 |
| inclination: | 97.2834° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 160.4557° |
| argument of perigee: | 56.5623° |
| revolutions per day: | 15.75323714 |
| mean anomaly at epoch: | 303.5787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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