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 63087U 26145.35927575 +.00000000 +00000-0 +17350-3 0 00007
2 63087 70.0004 161.2541 0004433 264.3959 95.6694 14.98335761 05
| Epoch (UTC): | 25 May 2026 08:37:21 |
| Eccentricity: | 0.0004433 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.2541° |
| argument of perigee: | 264.3959° |
| revolutions per day: | 14.98335761 |
| mean anomaly at epoch: | 95.6694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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