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 61761U 26145.50597007 +.00000000 +00000-0 +57234-3 0 00009
2 61761 97.2960 21.5451 0005373 19.4249 340.7210 15.55069694 08
| Epoch (UTC): | 25 May 2026 12:08:35 |
| Eccentricity: | 0.0005373 |
| inclination: | 97.2960° |
| perigee height: | 398 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 21.5451° |
| argument of perigee: | 19.4249° |
| revolutions per day: | 15.55069694 |
| mean anomaly at epoch: | 340.7210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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