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 61877U 26144.85165036 +.00000000 +00000-0 -84363-5 0 00003
2 61877 53.1596 341.0393 0000930 90.2497 269.8627 15.69720767 06
| Epoch (UTC): | 24 May 2026 20:26:22 |
| Eccentricity: | 0.0000930 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 341.0393° |
| argument of perigee: | 90.2497° |
| revolutions per day: | 15.69720767 |
| mean anomaly at epoch: | 269.8627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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