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 58905U 26145.37050361 +.00000000 +00000-0 +20389-3 0 00008
2 58905 49.9945 99.7628 0005590 303.9148 56.1258 14.83161846 06
| Epoch (UTC): | 25 May 2026 08:53:31 |
| Eccentricity: | 0.0005590 |
| inclination: | 49.9945° |
| perigee height: | 615 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 99.7628° |
| argument of perigee: | 303.9148° |
| revolutions per day: | 14.83161846 |
| mean anomaly at epoch: | 56.1258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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