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 52380U 26145.42621036 +.00000000 +00000-0 +11795-3 0 00009
2 52380 53.2120 194.6675 0001142 78.1131 281.9989 15.08838399 00
| Epoch (UTC): | 25 May 2026 10:13:44 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.6675° |
| argument of perigee: | 78.1131° |
| revolutions per day: | 15.08838399 |
| mean anomaly at epoch: | 281.9989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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