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 63880U 26145.41630343 +.00000000 +00000-0 +99134-4 0 00000
2 63880 70.0022 41.1036 0002769 265.5354 94.5488 14.98332806 09
| Epoch (UTC): | 25 May 2026 09:59:28 |
| Eccentricity: | 0.0002769 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1036° |
| argument of perigee: | 265.5354° |
| revolutions per day: | 14.98332806 |
| mean anomaly at epoch: | 94.5488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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