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 56282U 26087.76103264 +.00000000 +00000-0 +18031-2 0 00003
2 56282 98.8553 99.9223 0067914 224.9741 134.5923 14.20598408 01
| Epoch (UTC): | 28 March 2026 18:15:53 |
| Eccentricity: | 0.0067914 |
| inclination: | 98.8553° |
| perigee height: | 774 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 99.9223° |
| argument of perigee: | 224.9741° |
| revolutions per day: | 14.20598408 |
| mean anomaly at epoch: | 134.5923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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