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 63877U 26145.14107973 +.00000000 +00000-0 +30827-3 0 00007
2 63877 70.0022 41.7416 0002724 269.4715 90.6132 14.98338978 07
| Epoch (UTC): | 25 May 2026 03:23:09 |
| Eccentricity: | 0.0002724 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.7416° |
| argument of perigee: | 269.4715° |
| revolutions per day: | 14.98338978 |
| mean anomaly at epoch: | 90.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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