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 56995U 26145.57126112 +.00000000 +00000-0 +14650-3 0 00009
2 56995 97.8224 294.9780 0010952 262.5154 97.4836 15.20196050 05
| Epoch (UTC): | 25 May 2026 13:42:36 |
| Eccentricity: | 0.0010952 |
| inclination: | 97.8224° |
| perigee height: | 498 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 294.9780° |
| argument of perigee: | 262.5154° |
| revolutions per day: | 15.20196050 |
| mean anomaly at epoch: | 97.4836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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