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 65898U 26145.34026392 +.00000000 +00000-0 +65185-3 0 00004
2 65898 53.1601 14.3300 0001520 91.7532 268.3645 15.34414646 02
| Epoch (UTC): | 25 May 2026 08:09:58 |
| Eccentricity: | 0.0001520 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.3300° |
| argument of perigee: | 91.7532° |
| revolutions per day: | 15.34414646 |
| mean anomaly at epoch: | 268.3645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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