▸Orbital parameters

Orbit class	SSO
Inclination	97.3962°
Eccentricity	0.0008658
Period	94.6 min
Apogee	504 km
Perigee	492 km
Mean motion	15.22637132 rev/day
RAAN	80.0436°
Arg of perigee	85.3274°
Mean anomaly	274.8951°
B*	1.8171e-4
Rev at epoch	7,280

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 63234U 25052AA 26187.65927035 .00004161 00000-0 18171-3 0 9996

2 63234 97.3962 80.0436 0008658 85.3274 274.8951 15.22637132 72808

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TOMORROW-S5",
  "OBJECT_ID": "2025-052AA",
  "EPOCH": "2026-07-06T15:49:20.958+00:00",
  "MEAN_MOTION": 15.22637132,
  "ECCENTRICITY": 0.0008658,
  "INCLINATION": 97.3962,
  "RA_OF_ASC_NODE": 80.0436,
  "ARG_OF_PERICENTER": 85.3274,
  "MEAN_ANOMALY": 274.8951,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63234,
  "REV_AT_EPOCH": 7280,
  "BSTAR": 0.00018171,
  "MEAN_MOTION_DOT": 0.00004161,
  "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	TOMORROW-S5
Operator	Tomorrow.io (The Tomorrow Companies Inc.)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia 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/63234

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