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 68281U 26145.57587367 +.00000000 +00000-0 +51643-3 0 00006
2 68281 53.1576 322.7715 0001017 88.3151 271.7966 15.30196458 06
| Epoch (UTC): | 25 May 2026 13:49:15 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.7715° |
| argument of perigee: | 88.3151° |
| revolutions per day: | 15.30196458 |
| mean anomaly at epoch: | 271.7966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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