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 56953U 26145.35333807 +.00000000 +00000-0 +27379-3 0 00002
2 56953 97.6205 286.5995 0008582 44.0436 316.1490 15.37233882 03
| Epoch (UTC): | 25 May 2026 08:28:48 |
| Eccentricity: | 0.0008582 |
| inclination: | 97.6205° |
| perigee height: | 448 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 286.5995° |
| argument of perigee: | 44.0436° |
| revolutions per day: | 15.37233882 |
| mean anomaly at epoch: | 316.1490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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