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 68542U 26145.60548101 +.00000000 +00000-0 +65287-3 0 00002
2 68542 53.1612 5.1274 0001608 78.1061 282.0122 15.34409240 01
| Epoch (UTC): | 25 May 2026 14:31:53 |
| Eccentricity: | 0.0001608 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 5.1274° |
| argument of perigee: | 78.1061° |
| revolutions per day: | 15.34409240 |
| mean anomaly at epoch: | 282.0122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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