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 53801U 26145.35397128 +.00000000 +00000-0 -13053-4 0 00003
2 53801 53.2132 279.7134 0000713 35.7217 324.3823 15.08823261 05
| Epoch (UTC): | 25 May 2026 08:29:43 |
| Eccentricity: | 0.0000713 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 279.7134° |
| argument of perigee: | 35.7217° |
| revolutions per day: | 15.08823261 |
| mean anomaly at epoch: | 324.3823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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