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 61253U 26145.40997659 +.00000000 +00000-0 +19997-4 0 00006
2 61253 53.1599 38.2504 0000936 91.1739 268.9386 15.69714349 02
| Epoch (UTC): | 25 May 2026 09:50:21 |
| Eccentricity: | 0.0000936 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 38.2504° |
| argument of perigee: | 91.1739° |
| revolutions per day: | 15.69714349 |
| mean anomaly at epoch: | 268.9386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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