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 25394U 26088.17647689 +.00000000 +00000-0 +10235-3 0 00002
2 25394 98.9361 60.2518 0001852 36.8408 323.2897 14.25098250 08
| Epoch (UTC): | 29 March 2026 04:14:07 |
| Eccentricity: | 0.0001852 |
| inclination: | 98.9361° |
| perigee height: | 807 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 60.2518° |
| argument of perigee: | 36.8408° |
| revolutions per day: | 14.25098250 |
| mean anomaly at epoch: | 323.2897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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