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 68697U 26145.63743757 +.00000000 +00000-0 +34905-3 0 00003
2 68697 97.6657 221.2908 0016711 139.8415 220.4052 15.09895568 00
| Epoch (UTC): | 25 May 2026 15:17:54 |
| Eccentricity: | 0.0016711 |
| inclination: | 97.6657° |
| perigee height: | 525 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 221.2908° |
| argument of perigee: | 139.8415° |
| revolutions per day: | 15.09895568 |
| mean anomaly at epoch: | 220.4052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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