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 53928U 26145.50853756 +.00000000 +00000-0 +87213-5 0 00003
2 53928 53.2133 319.1639 0001205 101.3949 258.7178 15.08834057 02
| Epoch (UTC): | 25 May 2026 12:12:17 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.1639° |
| argument of perigee: | 101.3949° |
| revolutions per day: | 15.08834057 |
| mean anomaly at epoch: | 258.7178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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