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 63094U 26145.49697794 +.00000000 +00000-0 +17175-3 0 00002
2 63094 70.0006 160.9341 0004412 264.9939 95.0717 14.98339408 02
| Epoch (UTC): | 25 May 2026 11:55:38 |
| Eccentricity: | 0.0004412 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.9341° |
| argument of perigee: | 264.9939° |
| revolutions per day: | 14.98339408 |
| mean anomaly at epoch: | 95.0717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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