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 61514U 26145.44109720 +.00000000 +00000-0 +12287-4 0 00009
2 61514 53.1583 145.9217 0001008 73.9450 286.1661 15.30191046 00
| Epoch (UTC): | 25 May 2026 10:35:10 |
| Eccentricity: | 0.0001008 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 145.9217° |
| argument of perigee: | 73.9450° |
| revolutions per day: | 15.30191046 |
| mean anomaly at epoch: | 286.1661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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