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 62395U 26145.04135487 +.00000000 +00000-0 +56638-3 0 00009
2 62395 44.9964 26.4139 0006227 152.9669 207.1547 15.46399277 02
| Epoch (UTC): | 25 May 2026 00:59:33 |
| Eccentricity: | 0.0006227 |
| inclination: | 44.9964° |
| perigee height: | 423 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 26.4139° |
| argument of perigee: | 152.9669° |
| revolutions per day: | 15.46399277 |
| mean anomaly at epoch: | 207.1547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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