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 62068U 26145.46748610 +.00000000 +00000-0 +21408-2 0 00006
2 62068 53.1572 52.6744 0001007 56.9854 303.1260 15.69814439 05
| Epoch (UTC): | 25 May 2026 11:13:10 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1572° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 52.6744° |
| argument of perigee: | 56.9854° |
| revolutions per day: | 15.69814439 |
| mean anomaly at epoch: | 303.1260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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