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 63230U 26145.43855624 +.00000000 +00000-0 +15141-3 0 00007
2 63230 97.3935 40.8138 0023534 127.5394 232.7989 15.27571707 06
| Epoch (UTC): | 25 May 2026 10:31:31 |
| Eccentricity: | 0.0023534 |
| inclination: | 97.3935° |
| perigee height: | 467 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 40.8138° |
| argument of perigee: | 127.5394° |
| revolutions per day: | 15.27571707 |
| mean anomaly at epoch: | 232.7989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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