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 52378U 26145.57616426 +.00000000 +00000-0 +51271-4 0 00003
2 52378 53.2115 203.9662 0001243 74.1336 285.9793 15.08831514 05
| Epoch (UTC): | 25 May 2026 13:49:40 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 203.9662° |
| argument of perigee: | 74.1336° |
| revolutions per day: | 15.08831514 |
| mean anomaly at epoch: | 285.9793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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