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 00871U 26088.17728015 +.00000000 +00000-0 +10070-3 0 00005
2 00871 79.8946 156.2281 0085576 359.8436 0.2683 14.00657057 09
| Epoch (UTC): | 29 March 2026 04:15:17 |
| Eccentricity: | 0.0085576 |
| inclination: | 79.8946° |
| perigee height: | 829 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 156.2281° |
| argument of perigee: | 359.8436° |
| revolutions per day: | 14.00657057 |
| mean anomaly at epoch: | 0.2683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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