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 63387U 26145.16581845 +.00000000 +00000-0 +45764-3 0 00005
2 63387 53.1580 54.7252 0001095 87.4301 272.6825 15.30206490 06
| Epoch (UTC): | 25 May 2026 03:58:46 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.7252° |
| argument of perigee: | 87.4301° |
| revolutions per day: | 15.30206490 |
| mean anomaly at epoch: | 272.6825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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