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 56072U 26145.58522222 +.00000000 +00000-0 -12815-3 0 00000
2 56072 87.8988 263.6987 0001689 96.4465 263.6858 13.15550018 06
| Epoch (UTC): | 25 May 2026 14:02:43 |
| Eccentricity: | 0.0001689 |
| inclination: | 87.8988° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6987° |
| argument of perigee: | 96.4465° |
| revolutions per day: | 13.15550018 |
| mean anomaly at epoch: | 263.6858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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