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 63642U 26145.45214352 +.00000000 +00000-0 +10134-2 0 00009
2 63642 42.9984 291.9632 0000534 292.5163 67.5632 15.27607282 00
| Epoch (UTC): | 25 May 2026 10:51:05 |
| Eccentricity: | 0.0000534 |
| inclination: | 42.9984° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.9632° |
| argument of perigee: | 292.5163° |
| revolutions per day: | 15.27607282 |
| mean anomaly at epoch: | 67.5632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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