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 58102U 26145.49953622 +.00000000 +00000-0 +10720-4 0 00001
2 58102 53.1590 168.6110 0001047 91.0262 269.0859 15.30192338 00
| Epoch (UTC): | 25 May 2026 11:59:19 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1590° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.6110° |
| argument of perigee: | 91.0262° |
| revolutions per day: | 15.30192338 |
| mean anomaly at epoch: | 269.0859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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