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 61249U 26145.42949894 +.00000000 +00000-0 +17042-4 0 00000
2 61249 53.1595 37.6494 0000878 96.2049 263.9069 15.69710129 04
| Epoch (UTC): | 25 May 2026 10:18:28 |
| Eccentricity: | 0.0000878 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 37.6494° |
| argument of perigee: | 96.2049° |
| revolutions per day: | 15.69710129 |
| mean anomaly at epoch: | 263.9069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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