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 52355U 26145.59364253 +.00000000 +00000-0 +31721-4 0 00006
2 52355 53.2147 213.8852 0000975 92.9931 267.1172 15.08842968 04
| Epoch (UTC): | 25 May 2026 14:14:50 |
| Eccentricity: | 0.0000975 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 213.8852° |
| argument of perigee: | 92.9931° |
| revolutions per day: | 15.08842968 |
| mean anomaly at epoch: | 267.1172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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