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 63228U 26145.43540515 +.00000000 +00000-0 +22930-3 0 00008
2 63228 97.3950 38.5322 0003830 211.4419 148.6589 15.23301260 09
| Epoch (UTC): | 25 May 2026 10:26:59 |
| Eccentricity: | 0.0003830 |
| inclination: | 97.3950° |
| perigee height: | 493 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 38.5322° |
| argument of perigee: | 211.4419° |
| revolutions per day: | 15.23301260 |
| mean anomaly at epoch: | 148.6589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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