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 21712U 26087.70103529 +.00000000 +00000-0 +37929-3 0 00009
2 21712 89.2711 240.2156 0131404 160.8934 215.9071 14.25280403 01
| Epoch (UTC): | 28 March 2026 16:49:29 |
| Eccentricity: | 0.0131404 |
| inclination: | 89.2711° |
| perigee height: | 713 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 240.2156° |
| argument of perigee: | 160.8934° |
| revolutions per day: | 14.25280403 |
| mean anomaly at epoch: | 215.9071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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