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 61883U 26145.51767442 +.00000000 +00000-0 +79596-5 0 00004
2 61883 53.1593 337.3556 0000996 91.1169 268.9963 15.69711947 00
| Epoch (UTC): | 25 May 2026 12:25:27 |
| Eccentricity: | 0.0000996 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.3556° |
| argument of perigee: | 91.1169° |
| revolutions per day: | 15.69711947 |
| mean anomaly at epoch: | 268.9963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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