▸Orbital parameters

Orbit class	LEO
Inclination	44.9708°
Eccentricity	0.0006223
Period	92.9 min
Apogee	422 km
Perigee	414 km
Mean motion	15.49608608 rev/day
RAAN	157.0633°
Arg of perigee	99.0627°
Mean anomaly	261.0968°
B*	1.1046e-3
Rev at epoch	8,616

▸Two-line element set (TLE)

EPOCH Jul 5, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62394U 24247T 26186.35536948 .00062671 00000-0 11046-2 0 9995

2 62394 44.9708 157.0633 0006223 99.0627 261.0968 15.49608608 86169

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CROCUBE",
  "OBJECT_ID": "2024-247T",
  "EPOCH": "2026-07-05T08:31:43.923+00:00",
  "MEAN_MOTION": 15.49608608,
  "ECCENTRICITY": 0.0006223,
  "INCLINATION": 44.9708,
  "RA_OF_ASC_NODE": 157.0633,
  "ARG_OF_PERICENTER": 99.0627,
  "MEAN_ANOMALY": 261.0968,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62394,
  "REV_AT_EPOCH": 8616,
  "BSTAR": 0.0011046,
  "MEAN_MOTION_DOT": 0.00062671,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	CROCUBE
Operator	CroCube TeamHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	HR
Launch date	Dec 21, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/62394

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.