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 52115U 26145.24036742 +.00000000 +00000-0 -59651-5 0 00005
2 52115 53.2122 95.4699 0000828 96.4875 263.6211 15.08843546 05
| Epoch (UTC): | 25 May 2026 05:46:07 |
| Eccentricity: | 0.0000828 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 95.4699° |
| argument of perigee: | 96.4875° |
| revolutions per day: | 15.08843546 |
| mean anomaly at epoch: | 263.6211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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