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 25724U 26071.77427517 +.00000000 +00000-0 +13022-2 0 00009
2 25724 28.2233 214.1950 2130588 200.7710 149.1408 9.37496683 00
| Epoch (UTC): | 12 March 2026 18:34:57 |
| Eccentricity: | 0.2130588 |
| inclination: | 28.2233° |
| perigee height: | 1098 km |
| apogee height: | 5147 km |
| right ascension of ascending node: | 214.1950° |
| argument of perigee: | 200.7710° |
| revolutions per day: | 9.37496683 |
| mean anomaly at epoch: | 149.1408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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