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 52485U 26145.48235984 +.00000000 +00000-0 +22052-3 0 00002
2 52485 53.2151 64.3850 0001671 99.8297 260.2884 15.08804102 07
| Epoch (UTC): | 25 May 2026 11:34:35 |
| Eccentricity: | 0.0001671 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.3850° |
| argument of perigee: | 99.8297° |
| revolutions per day: | 15.08804102 |
| mean anomaly at epoch: | 260.2884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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