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 25414U 26088.20131427 +.00000000 +00000-0 +50440-3 0 00009
2 25414 44.9922 261.2861 0004183 267.7665 92.2705 14.39495809 06
| Epoch (UTC): | 29 March 2026 04:49:53 |
| Eccentricity: | 0.0004183 |
| inclination: | 44.9922° |
| perigee height: | 757 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 261.2861° |
| argument of perigee: | 267.7665° |
| revolutions per day: | 14.39495809 |
| mean anomaly at epoch: | 92.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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