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 25397U 26069.93422836 +.00000000 +00000-0 +66872-4 0 00002
2 25397 99.0028 60.2373 0002091 117.7101 242.4289 14.24406481 02
| Epoch (UTC): | 10 March 2026 22:25:17 |
| Eccentricity: | 0.0002091 |
| inclination: | 99.0028° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 60.2373° |
| argument of perigee: | 117.7101° |
| revolutions per day: | 14.24406481 |
| mean anomaly at epoch: | 242.4289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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