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 63098U 26145.39682133 +.00000000 +00000-0 +29230-3 0 00001
2 63098 70.0002 160.9770 0004131 267.9271 92.1415 14.98326559 04
| Epoch (UTC): | 25 May 2026 09:31:25 |
| Eccentricity: | 0.0004131 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.9770° |
| argument of perigee: | 267.9271° |
| revolutions per day: | 14.98326559 |
| mean anomaly at epoch: | 92.1415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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