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 68283U 26145.50738905 +.00000000 +00000-0 +83056-3 0 00000
2 68283 53.1585 323.0514 0000612 45.9947 314.1104 15.30219314 04
| Epoch (UTC): | 25 May 2026 12:10:38 |
| Eccentricity: | 0.0000612 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.0514° |
| argument of perigee: | 45.9947° |
| revolutions per day: | 15.30219314 |
| mean anomaly at epoch: | 314.1104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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