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 68072U 26145.47747731 +.00000000 +00000-0 +40701-3 0 00009
2 68072 53.1586 181.2005 0001130 81.6776 278.4355 15.34401866 02
| Epoch (UTC): | 25 May 2026 11:27:34 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 181.2005° |
| argument of perigee: | 81.6776° |
| revolutions per day: | 15.34401866 |
| mean anomaly at epoch: | 278.4355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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