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 68073U 26145.48799770 +.00000000 +00000-0 +49324-3 0 00001
2 68073 53.1595 181.2677 0001052 70.0577 290.0539 15.34406164 02
| Epoch (UTC): | 25 May 2026 11:42:43 |
| Eccentricity: | 0.0001052 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 181.2677° |
| argument of perigee: | 70.0577° |
| revolutions per day: | 15.34406164 |
| mean anomaly at epoch: | 290.0539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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