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 41877U 26145.61883788 +.00000000 +00000-0 +22215-3 0 00002
2 41877 98.7525 219.3071 0003047 126.9446 233.2010 14.21609111 01
| Epoch (UTC): | 25 May 2026 14:51:07 |
| Eccentricity: | 0.0003047 |
| inclination: | 98.7525° |
| perigee height: | 818 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 219.3071° |
| argument of perigee: | 126.9446° |
| revolutions per day: | 14.21609111 |
| mean anomaly at epoch: | 233.2010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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